obscuration in active galactic nuclei

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University of Kentucky UKnowledge eses and Dissertations--Physics and Astronomy Physics and Astronomy 2012 OBSCUTION IN ACTIVE GALACTIC NUCLEI Robert Nikua University of Kentucky, [email protected] is Doctoral Dissertation is brought to you for free and open access by the Physics and Astronomy at UKnowledge. It has been accepted for inclusion in eses and Dissertations--Physics and Astronomy by an authorized administrator of UKnowledge. For more information, please contact [email protected]. Recommended Citation Nikua, Robert, "OBSCUTION IN ACTIVE GALACTIC NUCLEI" (2012). eses and Dissertations--Physics and Astronomy. Paper 8. hp://uknowledge.uky.edu/physastron_etds/8

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Page 1: OBSCURATION IN ACTIVE GALACTIC NUCLEI

University of KentuckyUKnowledge

Theses and Dissertations--Physics and Astronomy Physics and Astronomy

2012

OBSCURATION IN ACTIVE GALACTICNUCLEIRobert NikuttaUniversity of Kentucky, [email protected]

This Doctoral Dissertation is brought to you for free and open access by the Physics and Astronomy at UKnowledge. It has been accepted for inclusionin Theses and Dissertations--Physics and Astronomy by an authorized administrator of UKnowledge. For more information, please [email protected].

Recommended CitationNikutta, Robert, "OBSCURATION IN ACTIVE GALACTIC NUCLEI" (2012). Theses and Dissertations--Physics and Astronomy.Paper 8.http://uknowledge.uky.edu/physastron_etds/8

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STUDENT AGREEMENT:

I represent that my thesis or dissertation and abstract are my original work. Proper attribution has beengiven to all outside sources. I understand that I am solely responsible for obtaining any needed copyrightpermissions. I have obtained and attached hereto needed written permission statements(s) from theowner(s) of each third‐party copyrighted matter to be included in my work, allowing electronicdistribution (if such use is not permitted by the fair use doctrine).

I hereby grant to The University of Kentucky and its agents the non-exclusive license to archive and makeaccessible my work in whole or in part in all forms of media, now or hereafter known. I agree that thedocument mentioned above may be made available immediately for worldwide access unless apreapproved embargo applies.

I retain all other ownership rights to the copyright of my work. I also retain the right to use in futureworks (such as articles or books) all or part of my work. I understand that I am free to register thecopyright to my work.

REVIEW, APPROVAL AND ACCEPTANCE

The document mentioned above has been reviewed and accepted by the student’s advisor, on behalf ofthe advisory committee, and by the Director of Graduate Studies (DGS), on behalf of the program; weverify that this is the final, approved version of the student’s dissertation including all changes requiredby the advisory committee. The undersigned agree to abide by the statements above.

Robert Nikutta, Student

Dr. Moshe Elitzur, Major Professor

Dr. Tim Gorringe, Director of Graduate Studies

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Obscuration in Active Galactic Nuclei

DISSERTATION

A dissertation submitted in partial fulllment of therequirements for the degree of Doctor of Philosophy in the

College of Arts and Sciencesat the University of Kentucky

By

Robert Nikutta

Lexington, Kentucky

Director: Dr. Moshe Elitzur, Professor of Physics and Astronomy

Lexington, Kentucky

2012

Copyright c© Robert Nikutta 2012

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ABSTRACT OF DISSERTATION

Obscuration in Active Galactic Nuclei

All classes of Active Galactic Nuclei (AGN) are fundamentally powered by accretionof gas onto a supermassive black hole. The process converts the potential energy ofthe infalling matter to X-ray and ultraviolet (UV) radiation, releasing up to several1012 solar luminosities.

Observations show that the accreting "central engines" in AGN are surroundedby dusty matter. The dust occupies a "torus" around the AGN which is comprisedof discrete clumps. If the AGN radiation is propagating through the torus on its wayto an observer, it will be heavily re-processed by the dust, i.e. converted from UV toinfrared (IR) wavelengths. Much of the information about the input radiation is lostin this conversion process while an imprint of the dusty torus is left in the releasedIR photons.

Our group was the rst to formulate a consistent treatment of radiative transferin a clumpy medium an important improvement over simpler models with smoothdust distributions previously used by researchers. Our code CLUMPY computesspectral energy distributions (SED) for any set of model parameters values. Fittingthese models to observed AGN SEDs allows us to determine important quantities,such as the torus size, the spatial distribution of clumps, the torus covering factor,or the intrinsic AGN luminosity. Detailed modeling also permits us to study thecomplex behavior of certain spectral features.

IR radiative transfer introduces degeneracies to the solution space: dierent pa-rameter values can yield similar SEDs. The geometry of the torus further exacerbatesthe problem. Knowing the amount of parameter degeneracy present in our modelsis important for quantifying the condence in data ts. When matching the mod-els to observed SEDs we must employ modern statistical methods. In my researchI use Bayesian statistics to determine the likely ranges of parameter values. I havedeveloped all tools required for tting observed SEDs with our large model database:the latest implementation of CLUMPY, the t algorithms, the Markov Chain MonteCarlo sampler, and the Bayesian estimator. In collaboration with observing groupswe have applied our methods to a multitude of real-life AGN.

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KEYWORDS: active galactic nuclei, infrared, clumpy dust tori, dust radiative trans-fer, Bayesian statistics

Student's Signature

Robert Nikutta

Date

1 August, 2012

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Obscuration in Active Galactic Nuclei

By

Robert Nikutta

Dr. Moshe ElitzurDirector of Dissertation

Dr. Tim Gorringe

Director of Graduate Studies

1 August, 2012Date

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[Scott's party is celebrating midwinter of the long Antarctic night, during the TerraNova Expedition, on June 22, 1911]

Whilst revelry was the order of the day within our hut, the elements without seemeddesirous of celebrating the occasion with equal emphasis and greater decorum. Theeastern sky was massed with swaying auroral light, the most vivid and beautiful dis-play that I had ever seen fold on fold the arches and curtains of vibrating luminosityrose and spread across the sky, to slowly fade and yet again spring to glowing life.

The brighter light seemed to ow, now to mass itself in wreathing folds in one quarter,from which lustrous streamers shot upward, and anon to run in waves through thesystem of some dimmer gure as if to infuse new life within it.

It is impossible to witness such a beautiful phenomenon without a sense of awe,and yet this sentiment is not inspired by its brilliancy but rather by its delicacy inlight and colour, its transparency, and above all by its tremulous evanescence of form.There is no glittering splendour to dazzle the eye, as has been too often described;rather the appeal is to the imagination by the suggestion of something wholly spiri-tual, something instinct with a uttering ethereal life, serenely condent yet restlesslymobile.

One wonders why history does not tell us of 'aurora' worshippers, so easily couldthe phenomenon be considered the manifestation of 'god' or 'demon.' To the littlesilent group which stood at gaze before such enchantment it seemed profane to returnto the mental and physical atmosphere of our house.

Robert Falcon Scott, "Scott's Last Expedition, Volume 1", 1913

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ACKNOWLEDGMENTS

My most sincere gratitude goes to my advisor Moshe Elitzur. I owe the successfuldissertation to his guidance, patience, wisdom, and to his brilliant mastery of physics.Praise from Moshe must be earned through hard work, but the joy of seeing himcompletely satised with one's work is immensely rewarding. I also want to thankMoshe for enabling hard-fought arguments about the science we were doing. Hetreated all discussions with a level of scrutiny that I aspire to. I feel that I grewsignicantly as a researcher through these discussions.

I would also like to thank Moshe and his wife Shlomit for being such warm andwelcoming friends. On so many occasions the invitations to their home gave me afeeling of home and family, while away from home.

Before joining UKY I had the enormous privilege to study with Achim Feldmeierat the Potsdam University in Germany. Achim introduced to me professionally con-ducted theoretical astronomy, and showed me through his tireless working ethics whatit takes to be a scientist. It is through his eort that I was able to come to UKY, forwhich I am immensely thankful, just as I am for his friendship.

I am indebted to the members of my PhD Advisory Committee, Professors IsaacShlosman, Ron Wilhelm, Dhananjay Ravat, Simon Bonner, Nancy Levenson andPinar Mengüç, who not only agreed to serve in this function, but provided veryvaluable support and suggestions that helped improving my dissertation. Specialthanks to Simon Bonner for his help with some of the statistics presented in thiswork.

I harbor deep gratitude towards Leslie Hunt and eljko Ivezi¢, from whom I havelearned a lot and who together with Moshe wrote reference letters during my searchfor a postdoc position. To the many collaborators I had the privilege and pleasure ofworking with I extend the warmest thank you. I feel very grateful to Andrés AsensioRamos who taught me many things about Bayesian inference.

I can not appreciate enough the help of and collaboration with my past andpresent colleagues Grant Thompson, Frank Heymann, Brian Oldeld, MridupawanDeka, Matt Sirocky (who together with his wife Emily welcomed me in the Statesfrom day one), and Loïc Chevallier (who opened my eyes when he introduced me toPython).

A deep thank you goes to my family for long-lasting, unbreakable support and forinspiration. To my parents and siblings for always believing in me, for encouragingme to go on, and to my grandmother for starting the re with my rst astronomybook as a boy. I cannot possibly mention everybody who became a friend over theyears. I am very grateful to all these wonderful companions both in Europe and inthe US. From the most recent years I want to thank specically Furea Kiuchi, whotalked sense into me on more than one occasion, Nandita Raha, who fortunately forme remains my friend despite our recurrent disagreement on certain issues, and toboth for patiently practicing my defense talk with me. Thanks go also to SunayanAcharya, who is probably the most well-read peer I know, and a constant source of

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curious discovery. Shout-outs go to all my other oce-mates and coee acionados.None of my work would have been possible without the administrative, organiza-

tional, and generous support of colleagues in the department oce. While I was inPotsdam, Mrs. Andrea Brockhaus was not only often the "last line of defense", butalso a close friend. In Lexington, the support of Eva Ellis, Carol Cottrill, MelissaMiller, Diane Riddell, Tammy Herring and others deserves much more praise andthanks than I can express in a few words. For his enormous support in all computer-related matters I want to thank Brian Doyle, quite simply the best sys-admin. Ialso want to express my sincere thanks to the Huaker Travel Scholarships Program,and to Prof. Lance DeLong who administers it. Through the generous support ofthe program I was able to participate in several international astronomy schools andconferences, and met incredible people in Toru«, Heidelberg, and Paris. To the Di-rectors of Graduate Studies, Professors Tom Troland, Joe Brill, and Tim Gorringe, Iwant to say thank you for welcoming me to the department, for their support, andfor occasional last-minute bail-outs.

Ning Kang, my dearest friend, has provided invaluable support, help, reassuranceand inquiry, warmth and patience with me over many years, I can never thank youenough for all this.

iv

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Table of Contents

Acknowledgments iii

List of Tables viii

List of Figures ix

Chapter 1 Introduction 11.1 Active Galactic Nuclei and dusty tori . . . . . . . . . . . . . . . . . 11.2 The clumpy torus model . . . . . . . . . . . . . . . . . . . . . . . . . 2

1.2.1 Cloud source functions . . . . . . . . . . . . . . . . . . . . . . 31.2.2 Brightness maps . . . . . . . . . . . . . . . . . . . . . . . . . 41.2.3 Torus spectral energy distributions . . . . . . . . . . . . . . . 5

1.3 CLUMPY model database and applications . . . . . . . . . . . . . . 7

Chapter 2 On the 10-micron silicate feature in Active Galactic Nuclei 92.1 Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 92.2 Silicate 10-Micron Emission Feature in QSO2 . . . . . . . . . . . . . 11

2.2.1 Observations . . . . . . . . . . . . . . . . . . . . . . . . . . . 122.2.2 Modeling . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 132.2.3 Results . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 132.2.4 Source Type . . . . . . . . . . . . . . . . . . . . . . . . . . . . 172.2.5 AGN Luminosity . . . . . . . . . . . . . . . . . . . . . . . . . 18

2.3 Feature Shape and Origin of 10-Micron Emission . . . . . . . . . . . 202.4 Spectral Properties of CLUMPY Models . . . . . . . . . . . . . . . . 262.5 Summary and Discussion . . . . . . . . . . . . . . . . . . . . . . . . . 302.6 Acknowledgments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 31

Chapter 3 Dusty models in WISE and Spitzer/IRAC photometric system forGalactic and extra-galactic sources 33

3.1 Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 333.2 Data and Sample Selection . . . . . . . . . . . . . . . . . . . . . . . . 34

3.2.1 WISE Mission . . . . . . . . . . . . . . . . . . . . . . . . . . . 343.2.2 Sample Selection . . . . . . . . . . . . . . . . . . . . . . . . . 35

3.3 Model Results . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 373.3.1 Smooth Dusty Spherical Shells . . . . . . . . . . . . . . . . . . 39

v

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3.3.1.1 Model Tracks for Smooth Spherical Distributions . . 403.3.2 Clumpy Dusty Tori . . . . . . . . . . . . . . . . . . . . . . . . 42

3.3.2.1 Clumpy color-color diagrams for WISE . . . . . . . 433.3.2.2 Clumpy color-color diagrams for Spitzer . . . . . . . 45

3.4 Discussion and Conclusions . . . . . . . . . . . . . . . . . . . . . . . 463.5 Acknowledgments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 47

Chapter 4 The CLUMPY model database: Bayesian analysis and degeneracies 494.1 Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 494.2 Fitting of SEDs . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 504.3 Multi-component SEDs . . . . . . . . . . . . . . . . . . . . . . . . . . 51

4.3.1 Addition of a blackbody component to torus SEDs . . . . . . 514.3.2 Over-tting . . . . . . . . . . . . . . . . . . . . . . . . . . . . 54

4.4 Bayesian inference . . . . . . . . . . . . . . . . . . . . . . . . . . . . 564.4.1 Bayes' Theorem . . . . . . . . . . . . . . . . . . . . . . . . . . 564.4.2 Likelihood . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 574.4.3 Marginalized posteriors . . . . . . . . . . . . . . . . . . . . . . 584.4.4 Markov chain Monte Carlo . . . . . . . . . . . . . . . . . . . . 584.4.5 Interpolation of the database . . . . . . . . . . . . . . . . . . 61

4.4.5.1 Interpolation by Articial Neural Network . . . . . . 614.4.5.2 Direct multi-dimensional interpolation . . . . . . . . 63

4.4.6 Application & Results . . . . . . . . . . . . . . . . . . . . . . 644.4.7 MCMC chain convergence . . . . . . . . . . . . . . . . . . . . 664.4.8 Y(q) sampling . . . . . . . . . . . . . . . . . . . . . . . . . . . 674.4.9 Parameter correlations . . . . . . . . . . . . . . . . . . . . . . 694.4.10 Theory selection . . . . . . . . . . . . . . . . . . . . . . . . . 71

4.5 Degeneracies . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 744.6 Acknowledgments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 79

Chapter 5 Conclusions 81

Appendix A Analytical scales of SED components 83

Appendix B CLUMPY integration procedures 85B.1 Integration in z-direction (1-D) . . . . . . . . . . . . . . . . . . . . . 85B.2 Integration of brightness maps (2-D) . . . . . . . . . . . . . . . . . . 87

B.2.1 Goal . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 87B.2.2 Monte-Carlo methods . . . . . . . . . . . . . . . . . . . . . . . 88B.2.3 Adaptive methods and the CUBA library . . . . . . . . . . . . 89B.2.4 Jacobian integral scaling . . . . . . . . . . . . . . . . . . . . . 90

Appendix C Kullback-Leibler Divergence 93C.1 Denition . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 93C.2 Constant prior . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 93

vi

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C.3 The meaning of DKL . . . . . . . . . . . . . . . . . . . . . . . . . . . 94C.3.1 (Piecewise) constant posterior . . . . . . . . . . . . . . . . . . 94C.3.2 Gaussian posterior . . . . . . . . . . . . . . . . . . . . . . . . 95C.3.3 Results . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 97

C.4 Limits . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 97C.5 Invariance under parameter transformations . . . . . . . . . . . . . . 98

Bibliography 100

Vita 112

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List of Tables

2.1 Clumpy parameters used in tting . . . . . . . . . . . . . . . . . . . 142.2 Properties of tted parameters for SST1721+6012 . . . . . . . . . . . 182.3 Properties of tted parameters for PG1211+143 . . . . . . . . . . . . 242.4 S10 statistics . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 30

3.1 Mean WISE colors of dierent source classes and Clumpy models . . 373.2 Sampled Clumpy parameter values . . . . . . . . . . . . . . . . . . . 44

4.1 Clumpy parameters used in tting . . . . . . . . . . . . . . . . . . . 50

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List of Figures

1.1 AGN unication and clumpy torus. . . . . . . . . . . . . . . . . . . . 21.2 The phases of a dust cloud illuminated directly by the AGN. . . . . . 31.3 10µm brightness map of a Clumpy torus. . . . . . . . . . . . . . . . 51.4 False-color images of a Clumpy torus. . . . . . . . . . . . . . . . . . 61.5 SEDs of a typical torus model. . . . . . . . . . . . . . . . . . . . . . . 7

2.1 SED of SST1721+6012. . . . . . . . . . . . . . . . . . . . . . . . . . . 142.2 Clumpy parameters well constrained by tting. . . . . . . . . . . . . 152.3 Less well constrained Clumpy parameters. . . . . . . . . . . . . . . . 162.4 Histograms of Pobsc. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 192.5 Histograms of the AGN bolometric luminosity. . . . . . . . . . . . . . 202.6 Apparent shift of the silicate feature peak in quasar PG1211+143. . . 212.7 Cloud column and 10µm emission through the best-t torus model for

PG1211+143. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 222.8 Distributions of S10 in several AGN samples . . . . . . . . . . . . . . 272.9 Comparison of S10 distributions in observations and Clumpy models. 29

3.1 Comparison of bandpasses for WISE and other major infrared surveys. 353.2 K-correction for quasars. . . . . . . . . . . . . . . . . . . . . . . . . . 363.3 Color-magnitude plots for dierent classes of WISE sources. . . . . . 373.4 SDSS g-r vs. u-g color-color diagram. . . . . . . . . . . . . . . . . . . 383.5 Extinction eciency proles, and SEDs of dusty shell models. . . . . 403.6 Model color-color tracks for spherical dusty shells around a central

black-body source. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 413.7 A comparison of source distribution in WISE color-color diagrams and

model predictions based on clumpy dust torus model. . . . . . . . . . 433.8 Comparison of models colors with WISE predictions. . . . . . . . . . 443.9 Color-color diagram of all Clumpy models in Spitzer's IRAC colors. 463.10 Average Ptype1 and f2 for all Clumpy models in Spitzer's IRAC colors. 47

4.1 Best ts to UV+IR SEDs of 25 type-1 quasars. . . . . . . . . . . . . 534.2 Fitting with models of increasing complexity. . . . . . . . . . . . . . . 554.3 MCMC example. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 594.4 Comparison of an original Clumpy model SED with its ANN-reproduced

version. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 624.5 Linear interpolation of logarithmic data. . . . . . . . . . . . . . . . . 64

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4.6 Example of MCMC sampling with the SED of Cygnus A. . . . . . . . 654.7 Y(q) fractions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 684.8 Sampling from Y (q) . . . . . . . . . . . . . . . . . . . . . . . . . . . . 694.9 2d-posteriors after tting Cyg A . . . . . . . . . . . . . . . . . . . . . 704.10 Fits to Spitzer data of PG1222+216. . . . . . . . . . . . . . . . . . . 724.11 Randomly drawn Clumpy SED without and with added noise. . . . 754.12 2d-histograms measuring the level of degeneracy in Clumpy parameters. 774.13 Histograms of the deviations of posterior medians from sampled pa-

rameter values. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 784.14 Full-width-at-half-maximum for all randomly sampled Clumpy models. 79

B.1 1D integration along a z-path. . . . . . . . . . . . . . . . . . . . . . . 86B.2 Adaptive 2D integration of brightness. . . . . . . . . . . . . . . . . . 90B.3 Area transformation. . . . . . . . . . . . . . . . . . . . . . . . . . . . 91

C.1 Uniform and piecewise-uniform priors/posterior. . . . . . . . . . . . . 94C.2 Kullback-Leibler divergence for a at prior, and a piecewise at / Gaus-

sian posterior. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 97C.3 Maximal width of a Gaussian posterior, assuming a at prior. . . . . 98C.4 Linear transformation of a probability density function. . . . . . . . . 99

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Chapter 1

Introduction

1.1 Active Galactic Nuclei and dusty tori

The various classes of Active Galactic Nuclei (AGN) are all powered by the accre-tion of gas onto a supermassive black hole (BH). Accretion converts a fraction of thepotential energy of the infalling matter to X-ray and UV radiation. Seyfert galax-ies (Seyfert, 1943) are prototypical AGN. Type-1 Seyferts show very broad spectralemission lines, indicative of high velocities of the gas that produces such lines, whileSeyfert-2s display only narrow lines. When broad emission lines were also detectedin the polarized light of Seyfert-2s (Antonucci and Miller, 1985), it was suggestedthat both classes intrinsically are of the same kind. A dusty torus obscures AGNlight along directions close to the equatorial plane, yet allows photons to escape inthe axial direction. The broad emission line signatures seen in polarized light fromtype-2 source is the radiation scattered toward us on dusty particles well above thetorus equatorial plane.

The light obscured by the torus emerges re-processed to infrared (IR) wavelengths.Observed dierences between type-1s and 2s are due to our dierent viewing of suchobjects. This AGN unication elegantly combines quasars, Seyfert galaxies, BL Lacobjects, etc., into one coherent picture. Figure 1.1a visualizes this paradigm (adaptedfrom Urry and Padovani, 1995).

Krolik and Begelman (1988) pointed out that due to dynamical considerations thedust must be contained in optically thick clouds rather than distributed smoothlythroughout the torus. Early models of torus spectral energy distributions (SED)nevertheless resorted to such smooth distributions (e.g. Pier and Krolik, 1992, 1993;Granato and Danese, 1994; Efstathiou and Rowan-Robinson, 1995; Granato et al.,1997; Schartmann et al., 2005; Fritz et al., 2006), simply because a consistent for-malism for radiative transfer in a clumpy medium was missing. With few exceptionsthese models failed to explain some curious observations made by modern instru-ments. The Spitzer Space Telescope added to the puzzles, among them the detectionof 10µm silicate emission in type-2 sources (Mason et al., 2009; Nikutta et al., 2009),or broadened and blue-shifted shapes of the emission feature in many type-1s (Sieben-morgen et al., 2005; Hao et al., 2005; Sturm et al., 2005). Another mystery was thelack of deep silicate absorption features in the SEDs of type-2 sources, contradict-ing the predictions of virtually all smooth-density models. IR interferometry alsorevealed later that both cool and much hotter dust co-exist at similar distances fromthe AGN (e.g.: Jae et al., 2004; Poncelet et al., 2006; Tristram et al., 2007; Rabanet al., 2009). This is irreconcilable with smooth dust distributions.

1

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(a)

Rd Ro

σ

i to observer

(b)

Figure 1.1: (a) AGN unication model with an anisotropically obscuring smooth-density dust torus (in orange) and the accreting black hole at the very center. In thisparadigm the source type depends on the observer's viewing angle (adaptation fromUrry and Padovani (1995)). (b) Cartoon of a clumpy torus comprising individualclouds (from Nenkova et al., 2008b). At all viewing angles an observer has a nitechance of not encountering any clouds at all, and thus seeing the AGN itself.

1.2 The clumpy torus model

In Nenkova et al. (2002, 2008a,b) a theory for radiative transfer in clumpy dust mediawas developed for the rst time. Fig. 1.1b shows a schematic cut through a clumpytorus. A number of discrete dusty clouds (each with an optical depth τV at visualwavelength λ = 0.55µm) is distributed in an axially-symmetric torus around a centralisotropic source of light (the AGN). The properties of the central light source, andthat of the chemical dust composition of the dust in the clouds are set; the AGNemission spectrum follows a broken-power law distribution (see Eq. 13 in Nenkovaet al. (2008a)), and the dust is a mixture of standard interstellar graphites (47%)and silicates (53%). The optical constants for the graphites are from Draine (2003),while the silicates are tabulated in Ossenkopf et al. (1992a) (hereafter OHM). Otherauthors sometimes use dierent tabulations of dust properties, but the eect on theoverall SED shapes is small in most cases. The dierences lie in the details, and willbe discussed in Chapter 2.

Beside the single-cloud optical depth, the model has ve further free parameters.Four pertain to the distribution of the clouds around the AGN. The average numberof clouds along a radial ray in the equatorial plane is N0 (Poisson-distributed aroundthis mean value). The number of clouds per radial ray decreases for directions that

2

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Tmin Tmax

α observer

Figure 1.2: The phases of a dust cloud illuminated directly by a central source, andobserved at dierent phase angles α. When α = 0 only the cooler side is visible,whereas at α = 180 the full hot face is seen. Figure from Nenkova et al. (2008a).

are inclined w.r.t the equatorial plane like a Gaussian of width σ (measured in de-grees from the equatorial plane). The distribution of the clouds in radial direction isgoverned by the index q of a power-law 1/rq. The torus has an outer radius whichis parametrized with Y , the ratio of outer to inner radii (the inner radius being setby an equilibrium temperature Tsub, above which dust will not sublimate, but ratherevaporate, because of the highly energetic UV-photons emerging from the centralsource.) For the standard silicate dust employed in our model this temperature isabout 1500 K. The nal free parameter is the viewing angle i under which the con-guration is being observed. It is measured in degrees from the torus rotational axis.

1.2.1 Cloud source functions

The dust clouds comprising the torus are illuminated by the central AGN. Sinceeach cloud is optically thick, even one cloud along the line of sight (LOS) blocks theview of the AGN entirely. If such a cloud were to be seen at an angle (away fromthe LOS AGNobserver), one would see parts of its hot, bright face, and parts ofits cooler, darker side (akin to the phases of the moon). Figure 1.2 visualizes suchcongurations. Therefore, for clouds that are directly illuminated by the AGN theemission spectrum of the cloud its source function (SFN) is determined by twovariables: the temperature at its hot surface (this is equivalent to the cloud's distancefrom the AGN), and by the phase angle α that the two lines of sight AGNobserverand AGNcloud include.

If a cloud itself does not have a clear view of the AGN, it is only heated by theradiation re-emitted by other clouds in its vicinity. The emission of such a "diusely"illuminated cloud can be approximated by calculating the SFN of a dust cloud em-bedded in an isotropic "radiation bath", whose wavelength-dependence is obtainedfrom averaging the emission spectra of surrounding clouds over all viewing angles.

Assuming that individual clouds in Clumpy are size-less "particles" (see, e.g.:Nenkova et al., 2008a,b, for a discussion), the wavelength-dependent SFN of a single

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cloud at any given point within the torus can be described as a combination of boththe local direct and diuse SFNs:

Sλ(r, α) = p Sdirλ (r, α) + (1− p) Sdiffλ (r), (1.1)

where p is the local probability that the cloud has a unobstructed view of the AGN.We have calculated a database of cloud SFNs for a range of distances r and phase

angles α (all SFN computations were performed with dusty (Ivezic et al., 1999)).This SFN database is then used in Clumpy when computing the SED of an entiretorus made of discrete clouds.

1.2.2 Brightness maps

Dening that the plane of the sky at which an observer looks is spanned by thecoordinate axes x, y, the computation of an entire torus SED requires that Clumpyobtains an image of the brightness distribution in the sky plane. Thus for everypoint (x, y) it must perform an integration along the z-direction through the toroidaldistribution of centrally-illuminated clouds, and at each point along the z-ray computethis function:

Hλ(x, y) =

∫z

Pesc,λ(z′, z)Sc,λ(z

′)NC(z′) dz. (1.2)

The integral is a product of three functions: the local cloud source function Sc,λfrom Eq. (1.1), the local number of clouds per unit length, NC, and the probabilityPesc,λ(z

′, z) that a photon generated at z′ will escape all the way along the remainderof the path without encountering any clouds. Please see Section B.1 in the Appendix,and the appendix in Nenkova et al. (2008b) for a more detailed explanation of thenecessary calculations.

Once the result of Eq. (1.2) is available for a set of positions that cover the x, y-plane well, an image of the brightness distribution of the object in the plane of skyhas been obtained. Figure 1.3 shows an example at 10µm, calculated for a torus withangular width σ=25, and viewed at an angle of 30 above the equatorial plane. Theinner dust-free cavity (with a radius of one dust sublimation radius) can be clearlyseen. The brightest regions seen in this image correspond to intensive 10µm emissionat the hot faces of directly illuminated clouds that are located at the far inner partof the torus. Although there are other clouds between the observer an the emittingclouds, many unobscured lines of sight exist, along which the photons can escape.This is a key feature of the clumpy treatment of radiative transfer, and in sharpcontrast to smooth-density models.

With the monochromatic brightness maps calculated for a number of wavelengths,alpha-compositing (see, e.g.: Porter and Du, 1984; Smith, 1995) of false-color imagesis possible. An example is shown in Figure 1.4. In the top row of panels the brightnessmaps at three dierent wavelengths are shown in false colors. From left to right thewavelengths are: 0.55µm (optical), 2.2µm (Near-IR, K-band), and 24µm (Far-IR).The torus conguration and the observer's perspective are similar to those in Fig. 1.3.

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Figure 1.3: 10µm brightness map computed with Clumpy of a torus seen at i = 60

from the axis, while the torus angular width is σ = 25 (measured from the equatorialplane). The most intense emission is therefore seen emerging from the bright facesof clouds on the far inner side of the torus. The inner dust-free cavity (with a radiusof one dust sublimation radius) can be clearly seen. The image edges are the axes ofthe plane of the sky.

Note how for the shortest wavelength the radiation is blocked (in the lower portionof the image) by dust clouds that are located between the observer and the source ofthe 0.55µm light. The intervening clouds are opaque to photons of this wavelength.On the other hand, longer-wavelength radiation can emerge freely from anywhere inthe torus, as can be seen from the symmetric appearance of the brightness map inthe right panel. The dust clouds are mostly transparent to Far-IR photons. It isalso evident that FIR emission is much more extended than optical emission, becausethe latter requires higher temperatures, and these only exist at closer distances tothe central source. The bottom panels of the gure show dierent compositions ofthe monochromatic brightness maps into multi-color images. The bottom right panelcombines all three maps.

1.2.3 Torus spectral energy distributions

Calculating brightness distributions for a comprehensive set of wavelengths, integrat-ing them over the x, y plane, and insuring correct normalization, we can compute theaverage spectral energy distribution (SED) of an entire torus. (See Section B.2 inthe Appendix for more details on the calculations.) Figure 1.5 shows as an examplethe SEDs of the torus model also used in Fig. 1.3, for 10 dierent viewing anglesi from 0 to 90. The SEDs show only the torus emission (no AGN contribution),and are normalized to the local bolometric AGN ux. The units are irrelevant, be-cause IR radiative transfer yields self-similar solutions (Ivezi¢ and Elitzur, 1997): ifthe total optical depth is held constant, the solution can not distinguish between

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0 100 200 300 400 500 600 700 800

0

100

200

300

400

500

600

700

800

0.55 µm

0 100 200 300 400 500 600 700 800

0

100

200

300

400

500

600

700

800

2.2 µm

0 100 200 300 400 500 600 700 800

0

100

200

300

400

500

600

700

800

24 µm

0 100 200 300 400 500 600 700 800

0

100

200

300

400

500

600

700

800

0.55 +2.2 µm

0 100 200 300 400 500 600 700 800

0

100

200

300

400

500

600

700

800

0.55 +24 µm

0 100 200 300 400 500 600 700 800

0

100

200

300

400

500

600

700

800

0.55 +2.2 +24 µm

Figure 1.4: False-color images of a Clumpy torus. The edges of each panel arethe two axes x and y in the plane of the sky. The labels are in arbitrary imagepixel units. Top row: Monochromatic brightness maps at three dierent wavelengthsare shown in false colors. From left to right the wavelengths are: 0.55µm (optical),2.2µm (Near-IR, K-band), and 24µm (Far-IR). Bottom row: The panels show dierentcompositions of the monochromatic brightness maps into multi-color images. Theright panel combines all three maps.

such extremes as a small light bulb embedded in a dusty atmosphere, but viewedfrom a short distance, and a powerful AGN shrouded in a massive dust shell, butviewed across intergalactic distances. The absolute scale is set by the luminosity ofthe illuminating source, but the spectral shape of the SEDs is independent of it.

One of the most striking features visible in the SEDs are the prominent spectralfeatures at 10µm and 18µm. They arise from resonant stretching and bending modesof the silicate molecules in the dust (Knacke and Thomson, 1973), and are proba-bly the most important spectral feature that can be used to characterize the torus,its conguration, and can also be used to distinguish between the two competingparadigms of smooth-density and clumpy AGN torus models.

The Clumpy formalism does away with AGN types that are solely based on theobserver's viewing angle. Instead, AGN visibility is set by the probability of havinga clear line-of-sight towards it. Even if an AGN is classied as type-2 by its emissionline spectrum, the 10µm silicate emission from hot cloud faces inside the torus stillhas a nite probability of reaching a distant observer though cloud-free channels.Such emission almost never occurs with smooth density models (an exception is Fritz

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10-1 100 101 102

wavelength λ [µm]

10-4

10-3

10-2

10-1

100

fluxλFλ/F

AG

N

Figure 1.5: SEDs of a typical torus model, for 10 dierent viewing angles i from 0

(top) to 90(bottom). Note how the 10µm silicate feature varies with viewing angle.

et al., 2006), yet it does in nature (e.g.: Teplitz et al., 2006; Mason et al., 2009; Nikuttaet al., 2009). Chapter 2 will go into much more detail on the properties of the 10µm

silicate feature and on the consequences of clumpiness.

1.3 CLUMPY model database and applications

We have made accessible to the community an extensive catalog of our Clumpy torusmodels1. In a growing number of publications the models have been used successfullyfor comparing observed data with model predictions (e.g.: Mason et al., 2006; AsensioRamos and Ramos Almeida, 2009; Ramos Almeida et al., 2009; Levenson et al., 2009;Landt et al., 2010; Deo et al., 2011; Malmrose et al., 2011b), and helped in explain-ing observations such as the initially puzzling Spitzer data mentioned in Section 1.1(Nikutta et al., 2009).

With the very large database of Clumpy models, calculated on a densely sampledgrid of model parameter values (in six dimensions, plus a wavelength dimension), wecan now undertake a wealth of exciting studies that involve the entire span of themodels. A search for models which best t the observed SED of an AGN is the rstapplication. I have made use of it in the research described in Chapters 2 and 4, andpostpone a deeper discussion until then.

In Chapter 3, from our forthcoming papers (Nikutta et al., 2012, 2013), we cal-

1www.pa.uky.edu/clumpy

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culated the spectral colors of all Clumpy models, and compared them both to pre-dictions, and to observations of thousands of dierent AGN made with the WISE

satellite (Wide-eld Infrared Survey Explorer).Like all models, the Clumpy formalism does have degeneracies in the parameter

space, arising both from the problem of IR radiative transfer (e.g.: Vinkovi¢ et al.,2003), and exacerbated by the geometry of the torus. Still a deeper physical un-derstanding of observations and of the likely parameter values can be obtained frommodeling observed AGN, and using Bayesian statistical methods to examine the levelsof degeneracy and condence in the inferred parameters. These are the main subjectin Chapter 4.

Copyright c© Robert Nikutta 2012

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Chapter 2

On the 10-micron silicate feature in Active Galactic Nuclei

This chapter is in most parts the published paper Nikutta, Elitzur, and Lacy (2009),

and a small erratum to it (Nikutta et al., 2010).

The 10µm silicate feature observed with Spitzer in active galactic nuclei (AGN)reveals some puzzling behavior. It (1) has been detected in emission in type 2 sources,(2) shows broad, at-topped emission peaks shifted toward long wavelengths in sev-eral type 1 sources, and (3) is not seen in deep absorption in any source observedso far. We solve all three puzzles with our clumpy dust radiative transfer formalism.Addressing (1), we present the spectral energy distribution (SED) of SST1721+6012,the rst type 2 quasar observed to show a clear 10µm silicate feature in emission.Such emission arises in models of the AGN torus only when its clumpy nature istaken into account. We constructed a large database of clumpy torus models andperformed extensive tting of the observed SED. We nd that the cloud radial dis-tribution varies as r−1.5 and the torus contains 24 clouds along radial equatorialrays, each with optical depth at visual ∼6080. The source bolometric luminosityis ∼3 · 1012 L. Our modeling suggests that . 35% of objects with tori sharingthese characteristics and geometry would have their central engines obscured. Thisrelatively low obscuration probability can explain the clear appearance of the 10µm

emission feature in SST1721+6012 together with its rarity among other QSO2. Inves-tigating (2) we also tted the SED of PG1211+143, one of the rst type 1 QSOs witha 10µm silicate feature detected in emission. Together with other similar sources,this QSO appears to display an unusually broadened feature whose peak is shiftedtoward longer wavelengths. Although this led to suggestions of non-standard dustchemistry in these sources, our analysis ts such SEDs with standard galactic dust;the apparent peak shifts arise from simple radiative transfer eects. Regarding (3)we nd additionally that the distribution of silicate feature strengths among clumpytorus models closely resembles the observed distribution, and the feature never occursdeeply absorbed. Comparing such distributions in several AGN samples we also showthat the silicate emission feature becomes stronger in the transition from Seyfert toquasar luminosities.

2.1 Introduction

Unied schemes of active galactic nuclei (AGN) require an obscuring dusty torusaround the central source, giving rise to a type 1 line spectrum when there is di-rect view of the central engine and type 2 characteristics when it is blocked (e.g.Antonucci, 1993; Urry and Padovani, 1995). The torus, which is comprised of dusty

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clouds that are individually optically thick (Krolik and Begelman, 1988), reprocessesthe radiation it absorbs into longer wavelengths, creating a distinct signature in theobserved infrared. Silicates, a major constituent of astronomical dust, reveal theirpresence through the spectral feature at 10 µm. Among type 1 AGN, QSOs displaythe feature in emission (Siebenmorgen et al., 2005; Hao et al., 2005; Sturm et al.,2005), while average SEDs of Seyfert 1 galaxies have either a at 10µm feature (Wuet al., 2009) or show it in mild absorption (Hao et al., 2007). Seyfert 2 galaxiesgenerally display an absorption feature with limited depth, much shallower than inultra-luminous IR galaxies (e.g. Hao et al., 2007; Levenson et al., 2007). An intriguingresult comes from the Spitzer observations of seven high-luminosity type 2 QSOs bySturm et al. (2006). While individual spectra appear featureless, the sample averagespectrum shows the 10µm feature in emission.

Heated dust will produce the feature in emission whenever it is optically thin.When the dust optical depth at 10 µm exceeds unity, the feature still appears inemission in viewing of the illuminated face of the dust but in absorption when thedust is between the observer and heating source. In the absence of a formalism forradiative transfer in clumpy media, early models of the AGN torus employed smoothdensity distributions instead (e.g. Pier and Krolik, 1992, 1993; Granato and Danese,1994; Efstathiou and Rowan-Robinson, 1995; Granato et al., 1997). These modelspredict that type 1 sources, where the observer has a direct view of the torus inner,heated face, will generally produce an emission feature, although some examples ofabsorption features do exist (Pier and Krolik, 1992; Efstathiou and Rowan-Robinson,1995). Type 2 viewing always produces an absorption feature, whose depth is quitelarge on occasion, much larger than ever observed. An emission feature is neverproduced from such viewing. A formalism for handling clumpy media was developedby Nenkova et al. (2002, 2008a) (hereafter N02 & N08a); the formalism holds forvolume lling factors as large as 10%. Their models show that a clumpy torus willnever produce a very deep absorption feature and that the feature displays a muchricher behavior than in smooth density models; in particular, type 1 viewing canproduce an absorption feature in certain models and type 2 viewing can lead to anemission feature in others (Nenkova et al., 2008b, N08b henceforth).

While the Sturm et al. (2006) data suggest the possibility of a 10µm emissionfeature in QSO2, the only unambiguous evidence for such a feature in a type 2 AGNwas presented recently for the Seyfert galaxy NGC 2110 (Mason et al., 2009). 1 Herewe present the rst unambiguous case of an emission feature in a type 2 quasar,SST1721+6012, and perform extensive tting of its spectral energy distribution (SED)with clumpy torus models.

The comparison of torus model predictions with observations is somewhat prob-lematic because the overwhelming majority of these observations do not properly

1Teplitz et al. (2006) have suggested a 10µm emission feature in the Spitzer spectrum of QSO2FSC10214+4724. The suggestion is problematic because the object's redshift is so high (z = 2.2856)that the 10µm feature was not fully in the spectral range of the IRS instrument. The rest-framespectrum is cut o around 12µm, before the continuum longward of the feature could be established.

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isolate the torus IR emission. Starburst emission is a well known contaminant inmany cases, and we selected SST1721+6012 for modeling precisely for this reasonas its spectrum seems free of starburst indicators. However, even IR from the im-mediate vicinity of the AGN may not always originate exclusively from the torus.High-resolution observations of NGC1068 by Cameron et al. (1993) and recently byMason et al. (2006) demonstrate that the torus contributes less than 30% of the 10µm

ux collected with apertures ≥ 1′′ in this object, with the bulk of this ux comingfrom dust in the ionization cones (Braatz et al. (1993) also found that at least 40% ofthe 12.4µm ux in this source do not originate from the torus). The signicance of IRemission from the narrow line region (NLR) was noted also by Schweitzer et al. (2008).However, because the dust in the ionization cones is optically thin, its IR emissionis isotropic and does not generate dierences between types 1 and 2. Observationsshow that such dierences do exist. In particular, the Hao et al. (2007) compilationof Spitzer IR observations shows a markedly dierent behavior for the 10µm featurebetween Seyfert 1 and 2 galaxies. Accepting the framework of the unication scheme,these dierences can be attributed only to the torus contribution. Thus it seems that,unfortunately, a general rule does not exist and the situation must be investigatedcase by case. Our aim here is to examine whether the torus contribution alone canreproduce the observed SED of SST1721+6012, yielding a range of possible parametervalues that describe the dusty cloud distribution in this source (2.2).

We also investigate the cause for apparent shifts of the silicate feature peakstowards long wavelengths (2.3). Such shifts have been reported for sources thatshow the 10µm feature in emission (Siebenmorgen et al., 2005; Sturm et al., 2005;Hao et al., 2005), and attributed to non-standard dust chemistry. However, theseshifts were never seen in absorption, suggestive of radiative transfer eects instead.Finally, in 2.4 we compare the observed distribution of silicate feature strengthsamong the Hao et al. (2007) sample of AGN with the synthetic distribution of featurestrengths in our database of clumpy torus model SEDs.

2.2 Silicate 10-Micron Emission Feature in QSO2

Although not expected in type 2 sources, possible detection of the 10µm emissionfeature was reported by Sturm et al. (2006). The feature was only identied after av-eraging the SEDs of a number of type 2 QSOs, which individually show no signicantindication of the feature. Recently Mason et al. (2009) presented the rst unequivocaldetection of an emission feature in an individual type 2 source, the Seyfert galaxyNGC 2110. We present the Spitzer SED of the type 2 quasar SST1721+6012 thatshows the 10µm and 18µm silicate features in emission. In this section we report onthe results of tting the SED of SST1721+6012 with clumpy torus models, and derivemultiple parameters characterizing the source.

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2.2.1 Observations

The source SSTXFLS J172123.1+601214 was rst identied as an AGN candidatein the Spitzer First Look Survey (FLS) by Lacy et al. (2004). It has a redshift ofz = 0.325, and was not present in the SDSS at that time. In 2007, Lacy et al. (2007a)categorized it as a type 2 quasar based on the presence of optical, narrow [N Roman5]emission lines and through emission line ratio diagnostics introduced by Baldwin et al.(1981b). In the same year Lacy et al. (2007b) presented, together with other sources,a wide-range SED for this source, including a mid-IR spectrum taken by the InfraredSpectrograph (IRS) aboard Spitzer.

The IRS observations (Astronomical Observation Request 1406768) were takenon 2005 August 14 in staring mode using the short and long low resolution modulesto obtain continuous coverage from 5.238 µm, and were passed through the S14.0version of the SSC pipeline. The signal-to-noise ratio varied through the spectrum,the deepest observations being targeted on the redshifted wavelengths of the strongspectral features expected to lie in the 715 µm range. In the short wavelengthmodule, two 14s ramps were taken in second order, and a single 60s ramp in rstorder. In the long wavelength module, two 30s ramps were taken in both rst andsecond order. The spectra from each module were optimally extracted using SPICE. 2

The resulting spectra were trimmed, combined, and resampled in constant energybins of ∆λ/λ ≈ 0.01, resulting in a spectrum ranging from 4.0 µm to 27.1 µm (restwavelength). Uncertainty estimates from SPICE were propagated through the processin the usual manner. For the tting we excluded a few data points at shorter andat longer wavelengths due to poor signal-to-noise ratio. Additionally, we make use oftwo photometric data points from the Infrared Array Camera (IRAC) component ofthe Spitzer First Look Survey (Lacy et al., 2005) at rest wavelengths of 2.7 µm and3.4 µm, both with very small intrinsic uncertainties, as they greatly help dening theshape of the SED in the regions of hot dust emission. Cross-calibration between IRSand IRAC is accurate to better than 10% (L. Yan, personal communication).

Despite a certain noisiness in the IRS spectrum, a clear presence of polycyclicaromatic hydrocarbon features (PAHs) can be safely excluded. Considering addition-ally its lack of a [Ne Roman2] emission line at 12.8 µm, the spectrum shows no signsof star formation. Furthermore, the SED seems free of other emission lines, withone disputable exception. Locally, the ux peaks around 10.5 µm, which coincideswith the [S Roman4] emission line at 10.51 µm reported to be found in 11 out of 12type 2 sources by Zakamska et al. (2008). This radiation, if indeed credited with anemission line, would stem from the AGN itself, but our spectrum does not show anyother lines originating from the AGN, like [Ne Roman3] at 15.5 µm and [Ne Roman5]at 14.3 µm. Within the frame of this work, we therefore attribute the peak ux at∼10.5 µm entirely to silicate emission.

2http://ssc.spitzer.caltech.edu/postbcd/spice.html

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2.2.2 Modeling

N02 & N08a describe an analytic formulation of radiative transfer in a clumpy, dustymedium heated by a radiation source. The formalism was implemented in the codeClumpy, which takes as input a toroidal distribution of point-like dust clouds arounda central source. The dust in each individual cloud has an optical depth τV , dened at0.55 µm, and standard ISM composition of 47% graphite with optical constants fromDraine (2003) and 53% cold silicates from Ossenkopf, Henning, and Mathis (1992a)(OHM hereafter). The dust sublimation temperature denes the torus inner radiusRd and is set to 1500 K. The cloud distribution is parametrized with the radial powerlaw 1/rq between Rd and the outer radius Y Rd, where q and Y are free parameters.Another free parameter is N0, the average number of clouds along a radial equatorialray. In polar direction the number of clouds per radial ray is characterized by aGaussian, so that at angle β from the equatorial plane it is N0 e

−(β/σ)2 , with σ thelast free parameter of the cloud distribution. The nal parameter is i, the observer'sviewing angle measured from the torus axis.

We employed Clumpy to produce a large database3 of model SEDs fλ = λFλ/FAGN ,with FAGN the total bolometric ux. The observations provide a set of uxes, F o

j ,at wavelengths λj, j = 1 . . . N . Our tting procedure involves searching the entiredatabase for the model that minimizes the error

E =1

N

√√√√ N∑j=1

(FAGN · fmj − λjF o

j

∆j

)2

, (2.1)

where ∆j are individual errors on the λjF oj , and f

mj are the model uxes at the same

set of wavelengths as the data. Each model SED is scaled by the factor FAGN thatminimizes E, determining the AGN bolometric ux for this model. Since the datadynamic range is only ≈ 3, the tting procedure can be safely executed in linearspace.

2.2.3 Results

We calculated E for all the Clumpy models whose parameters are listed in Table 2.1,resulting in a database of more than 4.7 million entries. This large set contains asa subset all the parameters that N08b found to be plausible. Figure 2.1 shows thedata and the best-tting Clumpy model. The two photometric IRAC points play acrucial role in the ts by expanding the data into the short wavelengths.

Although the model presented in Figure 2.1 produces the smallest nominal errorE, a number of other models have errors that dier from it only in the third signicantdigit. Because of the large degeneracy of the radiative transfer problem for heateddust, the SED is a poor constraint on the properties of the source; a meaningfuldetermination of model parameters requires also high-resolution imaging at various

3Models are available at http://www.pa.uky.edu/clumpy

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Table 2.1: Clumpy parameters used in tting

Parameter Sampled Values

q 0, 0.5, 1, 1.5, 2, 2.5, 3N0 1 - 25τV 5, 10, 20, 30, 40, 60, 80, 100, 150, 200, 300, 500σ 15, 20, 25, 30, 35, 40, 45, 50, 55, 60, 65, 70, 75, 80i 0, 10, 20, 30, 40, 50, 60, 70, 80, 90Y 2 - 5, 10, 20, 30, 40, 50, 60, 70, 80, 90, 100, 150, 200

Note: σ and i are measured in degrees.

100 101

rest wavelength [m]

10-1

100

F

[10

10Wm

3]

IRS spectrum

IRAC photometry

best fit model

5 10 15 20 25 [m]

0.5

1.0

1.5

2.0

F

[10

15Wm

2]

Figure 2.1: SED of SST1721+6012. Spitzer IRS data are shown in dark gray withthe errors in light gray shade. Two IRAC photometry points are marked with crosses.The black line shows the best-t Clumpy model, which produces an error Emin =0.212 (see Equation 2.1). Its parameters are q = 1.5, N0 = 3, τV = 80, σ = 20,Y = 30 and i = 60. The inset shows the data and the best t model using λFλ andlinear scales for a better display of the 10µm emission feature.

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0.5

1.0

0.5

1.0

fractionofaccep

tedmodels

0.5

1.0

0 1 2 3q

0.0

0.5

1.0

2 10 18

N0

100 200 300V

Er

5 %

Er

10 %

Er

15 %

Er

20 %

Figure 2.2: Bar diagrams of three Clumpy parameters well constrained by tting.From left to right, the columns correspond to q, N0, and τV . The parameters weresampled as listed in Table 2.1. Rows correspond, from top to bottom, to an increasingacceptance on the tting error relative to the best-t model, as marked on the right,with the resulting number of models increasing accordingly 199, 1691, 5210 and12854. The height of the bar at any value of a parameter is the fraction of all acceptedmodels.

wavelengths (e.g., Vinkovi¢ et al., 2003). The axially symmetric clumpy torus modelrequires a relatively large number of input parameters, further exacerbating the de-generacy problem. We dene Er = 100 · (E − Emin)/Emin as the relative deviationof a model from the best-t one. Then, 199 models have Er ≤ 5%, within a fractionof the minimal error Emin = 0.212, and the bar diagrams of these models are shownin the top rows of Figures 2.2 and 2.3 for each of the six parameters. All but two ofthese models share the same value of q = 1.5, indicating that this parameter can beconsidered well constrained. Similarly, for 90% of all models N0 is either 3 or 4, so thisparameter is only slightly less well constrained. The distributions of the parametersτV , σ and i are broader, but still show well dened peaks. For these parameters wecan only deduce a plausible range. In contrast, the parameter Y has a at distribu-tion that covers every sampled value Y ≥ 20; this parameter is undetermined, exceptfor the indication of a lower bound.

The choice Er ≤ 5% is of course arbitrary. Increasing slightly the range of ac-cepted models, the bar diagrams can be expected to remain peaked if the parametersare well constrained. The gures show that this is indeed the case for q and N0, whosedistributions remain reasonably peaked in spite of the large increase in the number of

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0.5

1.0

0.5

1.0

fractionofaccep

tedmodels

0.5

1.0

15 30 45 60 75

[deg]

0.0

0.5

1.0

0 30 60 90

i [deg]

50 100 150 200

Y

Er

5 %

Er

10 %

Er

15 %

Er

20 %

Figure 2.3: Same as Figure 2.2, but for the three less well constrained Clumpy

parameters σ, i, and Y . These distributions atten out more quickly with growingacceptance error.

accepted models (almost 13,000 are selected by the criterion Er ≤ 20%). To a lesserdegree, this is also the case for τV . In contrast, the distributions of σ and i, whichalso start out peaked, atten out signicantly as the acceptance criterion is relaxed,indicating that SED analysis lacks the predictive power to constrain these parametersin SST1721+6012. The only meaningful results are that, in all likelihood, σ . 50

and i ≤ 70, i.e., edge-on viewing is excluded. Furthermore, these parameters are notentirely independent of each other since a clear line of sight to the AGN can be ob-tained for dierent combinations of the two. In fact, the interdependence of σ, i, andto some degree N0 constitutes the greatest source of degeneracy within the clumpytorus SEDs. The nal parameter, the torus radial thickness Y , is undetermined. Asnoted already in N08b, the SEDs of models with a steep radial cloud distribution(q > 1) are insensitive to increasing Y because most of the clouds are concentratedin the torus inner region. The only constraint we can deduce is the lower boundY ≥ 10, indicating that the torus could be compact, in agreement with other AGNobservations (see N08b and references therein).

Table 2.2 summarizes the likely values constrained by tting. We cannot giveexact condence intervals since our distributions are not continuous. If a parameteris perfectly constrained, all models then have the same value. Denoting by H thefraction of models at the distribution peak value, such a parameter would have H =

1. On the other hand, a at distribution over the entire range of sampled valuesindicates a completely non-constrained parameter. If the number of parameter values

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in the sampled range is B, the height of each bar would then be 1/B. Introducew = H/B. A perfectly constrained parameter will have w = 1 (= H = B) whilefor an unconstrained parameter w = 1/B2, decreasing when the number of sampledvalues is increasing. We select as our sample the 1691 models with Er ≤ 10%. Whileadmittedly arbitrary, this selection ensures a strict acceptance criterion while stillgiving a statistically large sample. For each of the model parameters we identify theminimal interval around the distribution peak containing at least 90% of the sample'smodels. These ranges are listed in Table 2.2, together with the number of sampledvalues (bars) in these intervals, which is our measure of B. The last column lists thecorresponding values of w, reinforcing the perception conveyed by the bar diagramsregarding the degree of condence (or lack thereof) in each of the derived modelparameters.

This analysis shows that the radial cloud distribution in SST1721+6012 is wellconstrained at q = 1.5; although the 90% range contains also q = 1, 81% of the modelsare at q = 1.5. The likely value of N0 is similarly well constrained to the range 24;even though this parameter was densely sampled in steps of 1 all the way to 25, halfof the 50,000 best models fall within this narrow range. The third reasonably welldetermined parameter is τV ≈ 80, whose likely value is between 30 and 100. Notethat the values of these parameters for the best-tting model are q = 1.5, N0 = 3

and τV = 80, and that the close agreement with the distribution peaks is not a given in principle, the best-t model could fall anywhere inside the acceptable ranges.We have tried to put stronger constraints on the less well-dened parameters σ, i,and Y , by holding the values of the relatively well-constrained parameters xed atq = 1.5, N0 = 2 − 4, and τV = 60− 100. This had little eect on the distributionsof the unconstrained parameters, although the σ bar-diagrams became slightly morepeaked, showing a hint of greater preference for σ ≈ 15− 30. We conclude that it isimpossible to deduce σ, i, and Y for SST1721+6012 from SED analysis alone.

2.2.4 Source Type

In the standard form of the unication approach, the classication of an AGN as type1 or 2 is uniquely determined by the relation between the viewing angle i and thetorus angular thickness σ. In a clumpy medium, on the other hand, the source type isa matter of probability. Denote by N(i) the average number of clouds along a radialray at angle i, then

Pesc(i) = e−N(i) (2.2)

is the probability that a photon emitted by the AGN will escape the torus. Thesource has a probability Pesc(i) to appear as a type 1 AGN and Pobsc(i) = 1− Pesc(i)

as a type 2. With our Gaussian parametrization for the cloud angular distribution,

N(i) = N0 e− [(90−i)/σ]2 . (2.3)

The AGN type is probabilistic, and it depends on i, σ and N0.

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Table 2.2: Properties of tted parameters for SST1721+6012

Parameter Best Fit Peaka 90%-Rangeb Bc Hd we

q 1.5 1.5 1 1.5 2 0.81 0.40N0 3 3 2 4 3 0.42 0.14τV 80 80 30 100 5 0.30 0.06Y 30 20 20 200 11 0.13 0.01

σ 20 15 15 40 6 0.27 0.05i 60 50 0 60 7 0.16 0.02

Note: Statistical indicators for the sample of all 1691 models with Er ≤ 10% deviationfrom the best-t model.a Value of the parameter at the distribution peak.b Range around the peak containing at least 90% of the sample models.c Number of sampled values in the 90%-range.d Fraction of all accepted models at the distribution peak.e Measure of how well the parameter is constrained (see text); the closer w is to unitythe higher is the signicance of the determined value. The values for the last twoentries cannot be directly compared to all others since the range of both σ and i isnite whereas for all other parameters it is in principle unlimited.

Since SST1721+6012 is a type 2 quasar, the a priori expectation would be thatPobsc is large. We nd this not to be the case. The best-t model has Pobsc = 27%,and more than 75% of all models with Er ≤ 15% have Pobsc ≤ 33%. Figure 2.4displays the histograms of Pobsc for the models accepted at various tolerance levels,showing that the majority of models have Pobsc ≤ 10% (in the rst 3 panels). Suchlow probability would pose a problem if these were the numbers for a large sampleof type 2 sources. However, SST1721+6012 is a relatively rare type 2 quasar witha clear 10µm emission feature; of the more than twenty QSO2 with measured IRSEDs, NGC 2110 is the only other source with such unambiguous emission feature.The emission feature requires a direct line of sight to a signicant fraction of the hotsurfaces of directly illuminated clouds on the far inner side of the torus. Becauseobscuration of the AGN involves a single line of sight while the IR ux measurementsintegrate over many lines of sight, the relatively low values of Pobsc that emerge fromthe modeling are commensurate with the clear appearance of the 10µm emissionfeature in SST1721+6012 and its rarity among other QSO2 (see also 2.3).

2.2.5 AGN Luminosity

Since the central engine is obscured in SST1721+6012, a direct measurement of theAGN bolometric luminosity is impossible. However, the bolometric ux enters directlyinto the tting procedure (see Equation 2.1) as the scale factor that minimizes theerror in matching the model spectral shape with the data. The source luminosity

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0.0 0.5

Pobsc

0.0

0.1

0.2

0.3

0.4

0.5

0.6

0.7

0.8

fractionofaccep

tedmodels

Er 5 %(n=199)

0.0 0.5

Pobsc

Er 10 %(n=1691)

0.0 0.5

Pobsc

Er 15 %(n=5210)

0.0 0.5 1.0

Pobsc

Er 20 %(n=12854)

Figure 2.4: Histograms of Pobsc, the probability that the AGN is obscured by the torusin the Clumpy model (the probability that the model produces a type 2 source).Each panel corresponds to a dierent maximal acceptance error, as marked at thetop together with the corresponding number of models. Each bin width is 0.1 and itsheight is the fraction of all accepted models. The mean value in each panel, from leftto right, is 0.10, 0.11, 0.17 and 0.22

.

LAGN is then derived from its luminosity distance DL = 1.703Gpc, obtained fromthe redshift z = 0.325 for standard cosmological parameters (H0 = 70 km s−1 Mpc−1,ΩM = 0.3, at universe). The best-t model has L12 = LAGN/1012L = 0.90, andFigure 2.5 shows the distribution of logL12 derived for all tted models within agiven acceptance error. At the most restrictive level, all the models fall in the range1.1 ≤ L12 ≤ 6.5 and the mean value is 3.45, similar to the best-t model. Asthe acceptance becomes less restrictive, the range of accepted models extends toluminosities lower than 1012 L, but its upper boundary stays unchanged; the gurepanels for Er ≤ 10% and Er ≤ 20% for instance are very similar except for thepresence of more L < 1012L models in the latter. The reason is simple. Theluminosity scale factor is

∫Fλdλ, and as is evident from Figure 2.1, a large fraction

of the integral is contained at wavelengths that are missing from the data as they areshorter than the IRAC measurements. Model SEDs that drop precipitously beforethe IRAC points can still produce a small error estimate E by reasonably tting allother, longer wavelengths. Such models will be formally acceptablebut only becausethe short wavelength region, crucial for the luminosity determination, is so poorlysampled in the data. Observations at these short wavelengths will constrain betterthe SED, and provide a more accurate determination of L12. With the current data,our best estimate is L12 ' 3 with a likely range of 17.

Integrating the mid-infrared (MIR) luminosity only, Lacy et al. (2007b) nd

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-1.0 0.0

log L12

0.0

0.1

0.2

0.3

0.4

fractionofaccep

tedmodels

Er 5 %(n=199)

-1.0 0.0

log L12

Er 10 %(n=1691)

-1.0 0.0

log L12

Er 15 %(n=5210)

-1.0 0.0 1.0

log L12

Er 20 %(n=12854)

Figure 2.5: Histograms of the logarithm of the AGN bolometric luminosity,L12 = LAGN/1012L, derived from the scaling of each Clumpy model (see Equa-tion 2.1). Each panel corresponds to a dierent maximal acceptance error, as markedat the top together with the corresponding number of models. Each bin is 0.2 wide,and its height is the fraction of all accepted models. The mean value of L12 in eachpanel, from left to right, is 3.45, 2.71, 2.37 and 2.14.

LMIR = 0.25 · 1012 L. Richards et al. (2006) show that the bolometric correctionfrom the mid-infrared is about a factor of eight. With this correction, the earlierestimate gives L12 ∼ 2, in good agreement with the detailed Clumpy calculations.

2.3 Feature Shape and Origin of 10-Micron Emission

After many years in which it remained undetected in type 1 AGN, the 10µm featurewas nally discovered in emission in Spitzer observations (Siebenmorgen et al., 2005;Hao et al., 2005; Sturm et al., 2005). In addition, the 18µm feature appears inquite prominent emission. All three teams noted the large dierences with Galacticsources the 10µm emission feature in AGN is much broader, and in most casesits peak seems to be shifted to longer wavelengths, up to ∼11 µm. Analyzing thefeature with the simple approximation κλBλ(T ) (optically thin emission from dustat the single temperature T ), all three teams found signicant dierences betweenthe dust absorption coecient in AGN and the interstellar medium, suggestive ofa dierent mix of the silicate components. Signicantly, though, the shifts towardlonger wavelengths apparent in emission features were never reported in absorption;AGN absorption features reach their deepest level at the same wavelengths as Galacticsources, ∼9.8 µm. The dierent behavior of emission and absorption features suggeststhat the apparent peculiarities of AGN emission features do not arise from the dustcomposition, but rather from radiative transfer eects.

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0.04

0.12

0.20

0.28

0.36F

[Jy]

PG1211+143

CLUMPY model

spline w/o mid-points

spline w/ mid-points

0.00

0.20

0.40

F

Fcont

5 10 15 20 25 30

[m]

1.00

1.20

1.40

F/Fcont

Figure 2.6: Apparent shift of feature peak in quasar PG1211+143 as a radiative trans-fer eect. Top: The Spitzer data (black) show the 10µm and 18µm silicate featuresin emission. The SED of the best-t Clumpy model (within 830 µm) is shown ingreen; its parameters are q = 0, N0 = 5, τV = 20, σ = 25, Y = 20, i = 60. The modelreproduces observations that prompted suggestions for non-standard dust composi-tion. Two underlying continua are constructed as splines with (blue) and without(red) mid-range pivots over the 1414.5 µm inter-feature region. Middle: Continuum-subtracted uxes for each of the continua in the top panel. Bottom: The ux ratioF/Fcont for each continuum.

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x/Rd

20

0

20

y/R

d

(a1)

2 4 6

number of clouds

(a3)

5

0

5

y/R

d

(b1)

1 2

10m emission

(b3)

20 0 20

x/Rd

0

2

4

number

ofclouds

(a2)

5 0 5

x/Rd

0

1

210

mem

ission

(b2)

Figure 2.7: Cloud column (left) and 10µm emission (right) along viewing rays throughthe best-t torus model for PG1211+143 (see Table 2.3). (a1): Map of the cloudcolumn. Axes are linear displacements x/Rd and y/Rd from the central AGN, withRd the dust sublimation radius. The gray scale is linear, with white standing for zeroclouds and darker shades indicating higher cloud columns. (a2): One-dimensionalcut through the cloud number distribution in (a1) along the x-coordinate at y =0. (a3): Same as (a2), but vertically along the y-coordinate at x = 0. (b1): Thedistribution of 10µm emission emerging from the central 10Rd×10Rd. The gray scaleis linear, darker shades indicating higher 10µm emission. (b2): The 10µm emissionprole along the x-coordinate at y = 0, normalized to its central value. (b3): Sameas (b2), but vertically along the y-coordinate at x = 0.

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To further investigate this, we analyzed the Spitzer data of quasar PG1211+143,one of the sources in the original discovery paper of Hao et al. (2005), which showsboth silicate features in emission. While the data cover 535 µm, for the modeltting we employed only wavelengths between 8 and 30 µm. Fitting the shorterwavelengths with our torus models proved rather dicult in this source. The sameproblem arises in other PG quasars, where Mor et al. (2009) nd that high ux levelsat short wavelengths necessitate the addition of a hot dust component to the torusemission in their models (see also Netzer et al., 2007). Wavelengths longer than30 µm were omitted in the tting because of high noise levels. The top panel ofFigure 2.6 plots the observed SED of PG1211+143 between 5 and 30 µm in blackcolor and the SED of the best-t model in green. In addition to a prominent 18µm

feature, the displayed model shows a broad 10µm feature that reaches local peakemission at 11.6 µm. An analysis of the feature shape requires the constructionof an underlying continuum. Sirocky et al. (2008) discuss this problem in detailand show that the proper continuum denition requires a spline tted to the twowavelength regions shorter than the 10µm feature and longer than the 18µm feature,and in between them. This spline t to the model results is shown with blue colorin the gure. Although the central region, 1414.5 µm, is essential for a correctdenition of the continuum, it was missing from earlier analyses. The correspondingspline is plotted in red for comparison. The gure middle panel shows the continuum-subtracted ux in each case. The feature peaks at 10.0 µm in the properly constructedcontinuum, but has a at plateau between ∼9.811.6 µm that peaks nominally at10.5 µm in the traditional continuum. The bottom panel shows the ratio F/Fcont

for each continuum. Under the common parametrization with κλBλ(T ), the F/Fcont

curves would be taken as the actual dust absorption coecient. However, they arethe outcome of radiative transfer calculations with the standard OHM dust, whoseabsorption prole looks quite dierent; these articial absorption coecients aremuch atter than the peaked shape of the input κλ.

The reason for the peculiar shape of the emission feature is quite simple. Thefeature originates from the optically thin emitting layer on the bright surfaces ofclouds illuminated directly by the AGN. Absorption by other clouds encounteredon the way out toward the observer alters the feature's shape. This absorption isstrongest at the feature peak, where the absorption coecient is largest, and τV ∼20 is where single clouds become optically thick at that peak. When the generatedphotons encounter ∼1 cloud along the remaining part of the path toward the observer,the peak is absorbed while photons in the wings escape freely, eectively atteningthe shape of the feature. An increasing number of clouds along the path would absorbthe peak and the wings of the feature more strongly, producing a self-absorption dipin the feature's shape, and eventually suppressing the entire feature (see also Fig. 2in N08b). The apparent shift toward longer wavelengths arises from the interplaywith the shape of the rising continuum underneath the feature. It may be noted thatsuch apparent variations in the shape of the silicate emission feature in evolved stars

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Table 2.3: Properties of tted parameters for PG1211+143

Parameter Best Fit Peaka 90%-Rangeb Bc Hd we

Y 20 20 20 1 1.00 1.00q 0 0 0 0.5 2 0.61 0.30τV 20 20 20 30 2 0.50 0.25N0 5 6,7∗ 2 9 8 0.21 0.03σ 25 25 15 60 10 0.29 0.03i 60 0,10,20,40∗ 0 70 8 0.14 0.02

Note: Statistical indicators for the sample of all 28 models withrelative deviation Er ≤ 10% from the best-t model, and with N0 ≤10 (see text), listed in descending order of constraint. Footnotes afidentical to Table 2.2.∗Peak comprises multiple bins; all listed bins have equal heights.

prompted the suggestion of dust chemical evolution (Little-Marenin and Little, 1990;Stencel et al., 1990), but were similarly shown to reect radiative transfer eects(Ivezi¢ and Elitzur, 1995).

Table 2.3 summarizes the analysis of the distribution of all Clumpy models withtting errors within 10% of the best-t model. This prescription is identical to theone employed for SST1721+6012, but in the present case it yields only 38 modelsinstead of 1691. These models further break into two distinct groups with dierentranges of N0, the radial number of clouds in the equatorial plane. While 28 modelshave N0 ≤ 9, the other 10 fall in the N0 = 1618 range, with a large gap between thetwo groups. Because values of N0 larger than ∼10 are unlikely in general (see 3.4 inN08b), we exclude the ten models with N0 ≥ 16 from our sample.

As before, only three parameters are well constrained. The radial cloud distribu-tion is again well-constrained, but now it is at with q = 0. This leads to a stronglyconstrained torus thickness Y = 20, in sharp contrast with SST1721+6012 where Yis the least-well constrained parameter. All 28 models in the selected sample have thesame value of Y , although this probably reects our discrete sampling of parameterspace; there could be a small range around Y = 20, but 10 and 30 are clearly excluded.The cloud optical depth is well-constrained at τV ≈ 20−30. On the other hand, whilewell constrained for SST1721+6012, N0 is the least well constrained parameter here,with a likely range of 29 clouds.

As noted above, at-top emission features arise from absorption by a single cloudwith τV ∼ 20. As is evident from Table 2.3, all accepted models have τV ∼ 2030, butN0 is largely unconstrained. However, the average number of clouds along the line ofsight to the AGN (see Equation 2.3) falls within the narrow range 0 < N(i) ≤ 2.5 forall accepted models. To a certain degree, N(i) is a good proxy for the typical numberof clouds along lines of sight that pass close to the dust sublimation radius, wherethe 10µm emission is originating. In panel (a1) of Figure 2.7 we show the number ofclouds along all lines of sight through the best-t torus model. Panel (a2) shows a

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one-dimensional cut through the image, providing the prole of the number of cloudsper ray along the x-coordinate at y = 0. Due to the axial symmetry of the torus,this prole is symmetric with respect to x = 0, irrespective of the viewing angle.The signature of the central cavity is clearly visible in this prole: the cloud columnreaches a minimum of 2.4 at the center and stays close to this level for all x/Rd ≤ 1.It reaches a maximum of ≈ 6 clouds along rays roughly 10Rd away from the AGN.Panel (a3) shows the corresponding prole in the vertical direction at x = 0. Thesymmetry of this prole around y = 0 again reects the axial symmetry, which ensuresequal path lengths through the torus above and below the central line of sight.

While the number of clouds along two lines of sight displaced symmetrically fromthe center is equal, the illumination patterns of individual clouds as seen by theobserver can dier for the two, depending on the position angle in the plane of the sky.In panel (b1) we plot the two-dimensional distribution of the model 10µm emission forthe central region with size 10Rd×10Rd. Roughly 50% of the ux is detected withinthe inner 5Rd radius, and 70% of that fraction comes from the image upper half.This radiation originates from regions on the far inner face of the torus; no emissionoriginates from the near side, where the observer faces the dark sides of the clouds.Similar to panels (a2) and (a3), we plot in panels (b2) and (b3) proles of the 10µm

emission along the x and y directions. As expected, the horizontal prole in panel(b2) is symmetrical, clearly displaying the dust-free cavity at its center. On the otherhand, the shape of the vertical prole in (b3) reveals the asymmetry between theemission in the upper and lower halves. Despite equal cloud columns along viewinglines above and below the image center, the emission is not equal, owing to the stronganisotropy of single cloud emission. The 10µm emission originates from hot, brightsurfaces of clouds located on the torus far inner face. Clouds in the torus near side,which show their dark, cooler faces, only absorb the 10µm photons that were emittedon the torus far side.

Most clumpy torus models do not produce the apparent shift in peak emission.The shifts occur predominantly in models that have a small τV (. 20). Signicantly,τV ∼ 20 models are also the ones producing the most prominent 10µm emission fea-tures across the likely range of τV . As is evident from Fig. 16 in N08b, the emissionfeature strength decreases monotonically as τV increases up to τV ∼70; in some casesthe feature even switches to absorption for pole-on viewing. Therefore low-τV mod-els stand out in their feature strength and it is reasonable that such sources wouldbe preferentially selected in observations that looked to identify the 10µm silicateemission feature in AGN. Finally, it should be noted that the absorption coecientswidely used in the literature do not have their peaks at 9.8 µm. In the tabulationof Draine (2003), the feature peaks at 9.48 µm instead. The cold silicate dust ofOHM, which is the one used here, has its peak at 10.0 µm. The eect on the presentdiscussion is insignicant.

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2.4 Spectral Properties of CLUMPY Models

In addition to the detailed tting of the SST1721+6012 and PG1211+143 data, weinvestigated some other properties of the 10µm feature, comparing observations withgeneral properties displayed by the model database.

Hao et al. (2007) present a large compilation of Spitzer mid-IR spectra. Althougha loosely dened sample, it is the largest gathered thus far. For each source theymeasure the 10µm silicate feature strength S10 from

S10 = lnF (λ10)

Fcont(λ10), (2.4)

where F is the measured ux, Fcont is a continuum constructed underneath the 10µm

and 18µm silicate features (see Sirocky et al., 2008, for details; see also 2.3), and λ10

is the peak wavelength of the feature strength; emission features have a positive S10,absorption features a negative one.4 It may be noted that the specic prescription ofcontinuum construction modies, and can even reverse, the relative strengths of the10µm and 18µm features, as is also apparent from Figure 2.6; the ratio of the twostrengths is an important indicator of dust optical properties (Sirocky et al., 2008).

Removing all ULIRGs, the Hao et al. (2007) sample contains 21 QSOs, 38 Seyfert 1and 39 Seyfert 2 galaxies. The top panel of Figure 2.8 shows the histograms ofthe feature strengths for the three groups. The gure other panels show resultsfrom recent studies, which produced additional compilations of feature strengths:Thompson et al. (2009) compared a sample of Seyfert 1 galaxies with quasars, Wuet al. (2009) and Gallimore et al. (in preparation) analyzed Seyfert galaxies, bothtype 1 and 2, from the 12µm Galaxy Sample (Rush et al., 1993). While Wu et al. adoptthe original source classication of Rush et al., Gallimore et al. establish a dierentsource type in several cases, based on work published elsewhere. We employ the latterclassication in both panels (c) and (d), dispensing with all sources re-classied asLINERs or HII (star-forming) galaxies and conrming the Wu et al. suggestion thatthe re-classication of several sources has little eect on the statistical results of S10

measurements.In addition to the torus emission, the infrared radiation of many active galax-

ies contains a starburst contribution whose fractional strength varies from source tosource (e.g., Netzer et al., 2007). Removing the starburst component by subtractinga suitable template and leaving no PAH residuals is thus an important preliminarystep in the detailed SED analysis of many individual AGN (see, e.g., Mor, Netzer,and Elitzur, 2009). Note, however, that the two sources analyzed here in detail showno signs of ongoing star formation, either in the form of PAH emission or far-IR(FIR) emission. While PAH emission can contaminate the 10µm region in some in-dividual spectra, its overall impact on the averages of large samples seems minimal.

4The feature strengths of SST1721+6012 are S10 = 0.26 and S18 = 0.34 (for the 18µm feature).Both are uncertain to within ∼ ± 0.1. For the model shown in Figure 2.6, the feature strengthsdetermined from the blue curve are S10 = 0.26 and S18 = 0.21 (at 18.0 µm), and S10 = 0.33 andS18 = 0.21 (at 17.5 µm) from the red curve.

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0

5

10

15

sources

/bin

(a) Hao et al. 2007 QSO (21)

Sy1 (38)

Sy2 (39)

0

5

10

15

20

sources

/bin

(b) Thompson et al. 2009 QSO (20)

Sy1 (29)

0

5

10

sources

/bin

(c) Wu et al. 2009 Sy1 (27)

Sy2 (42)

-2-1.5-1-0.500.51

S10

0

5

10

sources

/bin

(d) Gallimore et al. (in prep.) Sy1 (27)

Sy2 (42)

Figure 2.8: Distributions of the 10µm silicate feature strength S10 (Equation 2.4) inseveral AGN samples. The bin size is 0.1. All ULIRGs present in the original sampleshave been removed. Measurements for QSOs are shown with gray bars, Seyfert 1swith dashed lines, and Seyfert 2s with solid lines. The number of sources of dierenttype is given in parentheses in the legend. (a): Spitzer sample by Hao et al. (2007).(b): Archival sample of type 1 sources by Thompson et al. (2009). Note the dierentscale. (c): Seyfert sources from the 12µm Galaxy Sample, presented by Wu et al.(2009), and (d) re-analyzed by Gallimore et al. (in preparation). Panel (c) containsonly sources also present in (d), and the source classication in both panels is adoptedfrom the latter.

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Netzer et al. (2007) subtract a starburst template from the average spectra of AGNwith and without strong FIR detections and nd that the MIR regions are hardlyaected by this subtraction in either case. In particular, their Figure 6 shows thatthe strength of the 10µm silicate feature barely changes. The analyses by Wu et al.(2009) and Gallimore et al. (in preparation) of the same data set provide an evenstronger evidence: The former ignores the potential starburst contribution while thelatter includes a PAH component, handled with the Pahfit tool (Smith et al., 2007).In spite of this dierence, the histograms in panels (c) and (d) of Figure 2.8 are quitesimilar, showing comparable lower and slightly increased upper limits on S10 and anoverall shape that is essentially the same.

Comparison of the histograms for type 1 sources in the panels of Figure 2.8 showsthat in moving from Seyfert to quasar luminosities the 10µm feature shifts to enhancedemission. This trend was noted earlier in Nenkova et al. (2008b; see 6.4), and theanalysis here veries this suggestion, giving it quantitative evidence. Nenkova et al.point out that the most likely explanation is that the number of clouds along radialrays is smaller in quasars than in Seyferts.

Grouping together the QSOs and Seyfert 1s of the Hao et al. (2007) sample,the top panel of Figure 2.9 shows the histograms and Table 2.4 lists the statisticalindicators of the S10 distributions in type 1 and 2 sources. Most sources exhibitrather small absolute values of S10. The histogram of type 1 sources is clearly shiftedtoward emission in comparison with type 2. Although the Hao et al. (2007) sources donot constitute a complete sample, the selection criteria were unrelated to the silicatefeature. The derived histograms can thus be reasonably considered representative ofthe dierences between types 1 and 2.

Our clumpy torus models should produce similar histograms if they bear a resem-blance to the IR emission from AGN. Such a comparison presents two fundamentaldiculties. First, the assignment of a given clumpy model to type 1 or 2 is not deter-ministic only a probability can be assigned. We handle this problem by dividingthe models according to the probability Pesc for an unobscured view of the AGN.The collection of models with Pesc > 0.5 can be expected to resemble the behavior ofthe type 1 population, those with Pesc < 0.5 type 2. The second problem is that theactual distribution of parameter values is unknown. Since we do not have any handleon these distributions, we decided to test the adequacy of histograms produced bya uniform sampling of the model parameters within the bounds deduced in N08b:0 ≤ q ≤ 3, N0 ≤ 15, 30 ≤ τV ≤ 100, 15 ≤ σ ≤ 60, and 10 ≤ Y ≤ 100. Sinceq was sampled here more thoroughly than in N08b, we use the full range listed inTable 2.1. The parameters were sampled in steps of 0.5, 1, 10, 5, 10, 10 for q, N0,τV , σ, Y , i, respectively. The bottom panel of Figure 2.9 shows the histograms ofS10 for all database models selected by these criteria. These distributions resemblethose of the observational sample, as is also evident from their statistical propertieslisted in Table 2.4. The 1σs and 2σs ranges of S10 given in the table contain sourcesand models within 1 and 2 standard deviations σs from the mean of each of the two

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0

1

2

3

sources/bin(norm

.) Hao et al. 2007 QSO + Sy1

Sy2

-2-1.5-1-0.500.51

S10

0

1

2

models/bin

(norm

.) CLUMPY Pesc > 0.5

Pesc < 0.5

Figure 2.9: Distributions of the 10µm silicate feature strength S10. The bin size is0.1 and each histogram is normalized to unit area. Top: Data from the Hao et al.(2007) sample. Dotted line shows type 1 sources (QSO and Seyfert 1 combined), solidline Seyfert 2s. Bottom: Histograms for 840,000 Clumpy models whose parametersmost likely correspond to physical values (see text). Models with escape probabilityPesc > 0.5 (likely type 1 source in a clumpy torus) are shown as dotted line, thosewith Pesc < 0.5 (likely type 2) as solid line. For statistical properties of all samplessee Table 2.4.

distributions. Leading to exclusion of only few sources and models at the very ends ofthe distributions, this additional selection has the eect of a much more meaningfulagreement of the two distribution widths, not spoiled by rare outliers. At the 2σslevel, rejected sources are just 3 type 1 and 2 Seyfert 2s, and among the sample ofmodels only 4% of those with Pesc > 0.5 and 6% with Pesc < 0.5 are excluded due tothis criterion.

Although the choice of uniform sampling of the model database is arbitrary, itproduces reasonable results. The reason is that, as noted already in N08a and N08b,clumpy models never produce very deep absorption features, in agreement with obser-vations. This limited range is reected in the histograms for any reasonable criteriaused for model selection from the database. The other main characteristic of theobserved histograms is the separation between type 1 and 2 sources, and this, too, isreproduced reasonably well by the models.

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Table 2.4: S10 statistics

Hao et al. (2007) Clumpy

source type QSO + Sy1 Sy2 Pesc > 0.5 Pesc < 0.5sample size 59 39 340,000 500,000

mean 0.03 -0.46 0.15 -0.33median 0.12 -0.34 0.12 -0.32σs 0.36 0.40 0.29 0.38

1σs-rangea -0.30, 0.37 -0.83, -0.06 -0.14, 0.44 -0.71, 0.042σs-rangeb -0.44, 0.40 -1.20, 0.29 -0.42, 0.73 -1.09, 0.42Note: Samples of AGN and of Clumpy models as in Figure 2.9.aRanges of 1 standard deviation σs from a sample's mean value.bThe 2-standard deviations range.

2.5 Summary and Discussion

Spitzer IR observations of AGNs have increased signicantly the number and qualityof SEDs for these objects and produced some puzzling results, especially with regardto the 10µm silicate feature. These include (1) detection of the feature in emissionin type 2 sources, (2) emission features with broad, at-topped peaks shifted towardlong wavelengths in several type 1 sources, and (3) absence of any deeply absorbedfeatures. None of these observations can be satisfactorily explained with smoothdensity torus models.

Here we have shown that clumpy torus models provide reasonable explanationsfor all three puzzles. To that end we have tted the Spitzer SEDs of two very dierentsources with our Clumpy models. One source, SST1721+6012, is the rst type 2QSO to show a clear 10µm emission feature. Our analysis provides a reasonable t ofthe SED with a model that shows the feature in emission. In contrast with smoothdensity models, where the AGN is either obscured or visible, our model produces asmall obscuration probability, Pobsc = 27%, for this type 2 source. This relatively lowprobability may explain why SST1721+6012 is the only source among more than 20type 2 QSOs with measured SEDs (see, e.g., Polletta et al., 2008) to show a clear10µm emission feature.

Addressing the second puzzle, PG1211+143 is one of the rst QSOs to display the10µm silicate feature in emission, a feature that is unexpectedly broad and apparentlyshifted to longer wavelengths. The original attempts to explain these propertiesinvoked non-standard chemical dust composition. Our modeling shows that the shiftsare only apparent and result from the attening of the feature peak by radiativetransfer in clumpy media. The feature is well reproduced by clumpy models withstandard dust. The third observational puzzle, lack of deep 10µm absorption featuresin any AGN, has already been shown to be a signature of clumpy dust distributions(Nenkova et al., 2002; Levenson et al., 2007; Sirocky et al., 2008; Nenkova et al.,2008a,b). Here we go a step further and produce the histogram of 10µm feature

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strength for a large sample of AGN Clumpy models. The result is in good qualitativeagreement with the sample observed by Hao et al. (2007). In particular, the medianvalues of both type 1 and type 2 observed distributions and their widths are wellreproduced by the model database.

The IR SED generally does not constrain very tightly the properties of dustysources the large degeneracy of the radiative transfer problem for heated dust iswell known (e.g., Vinkovi¢ et al., 2003). In the present case, the problem is furtherexacerbated by the clumpy nature of the dust distribution and the non-spherical ge-ometry. Our model database contains close to 5 million entries, and although thetting procedure eliminates most of them, many produce reasonable agreement withthe observations. In the case of SST1721+6012, close to 1,700 models with very dier-ent parameters deviate by no more than 10% from the best-t model. And while themuch higher quality of data in PG1211+143 greatly reduces the number of acceptablemodels, there are still 28 dierent ones that are practically indistinguishable in thequality of their ts. In the face of this degeneracy, we have developed a statisticalapproach to assess the meaningfulness of the various torus parameters derived fromthe ts. We nd that some parameters are well constrained in each case, while othersare not. In both sources the power law of the radial distribution (q) and the opti-cal depth of a single cloud (τV ) are well constrained, while the torus viewing angle(i) and its angular thickness (σ) are not. Both the cloud number (N0) and radialthickness (Y ) are well constrained in only one of the sources, a dierent one in eachcase. Asensio Ramos and Ramos Almeida (2009) have recently developed a dierent,novel approach to tackle the degeneracy problem. They interpolate the Clumpy

SEDs by means of an articial neural network function, allowing them to study theparameter distributions as if they were continuous, and employ Bayesian inferenceto determine the most likely set of parameters. Applying this method to a selectionof sources, Ramos Almeida et al. (2009) nd that the principal ability to constraindierent Clumpy parameters strongly depends on the individual source. We havealready begun an extensive comparison of the two approaches and will report ourndings elsewhere.

Although the SED alone is generally insucient for determining all the torusparameters with certainty, the success in resolving outstanding puzzling behavior ofthe 10µm feature in AGN is encouraging and enhances condence in the clumpy torusparadigm.

2.6 Acknowledgments

We are indebted to Jack Gallimore for kindly providing his measurements of silicatefeature strengths prior to publication and agreeing to their inclusion in Figure 2.8.We thank Lei Hao for providing her original data (included in Figures 2.8 and 2.9and Table 2.4), and Nancy Levenson for the SED of PG1211+143 (Figure 2.6). Wefurther thank Cristina Ramos Almeida, Eckhard Sturm and the anonymous refereefor valuable comments. ME acknowledges the support of NSF (AST-0807417) and

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NASA (SSC-40095). RN appreciates early PhD support by A. Feldmeier and DFG(Fe 573/3).

Copyright c© Robert Nikutta 2012

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Chapter 3

Dusty models in WISE and Spitzer/IRAC photometric system forGalactic and extra-galactic sources

The content in this chapter is largely from two papers in preparation, Nikutta, Nenkova,

Ivezi¢, and Elitzur (2012) and Nikutta, Messias, Nenkova, Ivezi¢, and Elitzur (2013).

The text and gures are contributed by all co-authors.

We present color-color tracks in WISE photometric system (3.4, 4.6, 12, and22 µm) based on radiative transfer calculations for two families of models: smoothspherical shells with various dust density distributions and chemical compositions,and clumpy dust torus models designed to model emission from active galactic nucleiand quasars. We compare our results with the distribution of Galactic and extra-galactic sources in various WISE color-color diagrams and nd that the observedstructure can be readily understood with the aid of these models.

3.1 Introduction

Radiation emitted at infrared wavelengths often carries unique information about as-tronomical sources due to two main reasons: dust extinction rapidly decreases withwavelength, and radiation from dust at temperatures below typical condensation tem-perature (∼1000 K) is predominantly emitted at infrared wavelengths. The pioneeringInfrared Astronomical Satellite (IRAS, launched in 1983) all-sky survey ushered inthe era of modern highly successful astronomical surveys1 (Neugebauer et al., 1984;Olnon et al., 1986). The IRAS survey provided unprecedented opportunity to classifythe infrared properties of about 350,000 astronomical objects using a homogeneousdata set obtained with a single facility (e.g. van der Veen and Habing 1988). Therecent Wide-eld Infrared Survey Explorer (WISE, launched in 2010) all-sky survey,thanks to sensitivity improvements of up to three orders of magnitude compared toIRAS, detected about 560 million objects (Wright et al., 2010).

WISE represents the next major step in the surveying and understanding of theinfrared sky. For example, data from the IRAS Point Source Catalog (PSC) showedthat certain Galactic objects tend to cluster in well-dened regions of IRAS color-color diagrams the same clustering is expected in WISE photometric system for asignicantly larger sample that probes a much larger volume of the Galaxy. Further-more, and perhaps more importantly, WISE data are deep enough for its catalogsto contain a very large number of extra-galactic sources, and they too are clusteredin well-dened regions of WISE color-color diagrams. Although IRAS also detected

1ADS returns over 11,000 papers which mention word IRAS in their abstract (as of June 1, 2012).

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some extra-galactic objects (for a review see Soifer et al. 1987), the WISE can beconsidered as a true infrared counterpart to modern optical surveys of extra-galacticsources, such as the Sloan Digital Sky Survey (SDSS, York et al. 2000).

The main aim of this paper is to present model color-color tracks for the WISEphotometric system which can be used to interpret the observed clustered source dis-tribution. We perform radiative transfer calculations for spherical shells with variousdust density distributions and chemical compositions, analogously to the IRAS-basedstudy by Ivezi¢ and Elitzur (2000). These models are applicable to objects such asasymptotic giant branch stars and various classes of young stellar objects. In addi-tion, we also present the model results for clumpy dust torus models which explainthe properties of infrared emission from AGN and quasars reasonably well (Nenkovaet al., 2002, 2008a,b).

In 3.2, we provide a brief summary of WISE data and samples of sources used indata vs. model comparison. A detailed description of models and comparison withWISE data is presented in 3.3, and our results are discussed and summarized in 3.4.

3.2 Data and Sample Selection

We begin with a brief overview of WISE mission. A more detailed discussion can befound in Wright et al. (2010) and at the WISE data release website2.

3.2.1 WISE Mission

WISE mapped the sky at 3.4, 4.6, 12, and 22 µm (see g. 3.1 for WISE bandpassesand their comparison to other major infrared surveys) with an angular resolutionof 6.′′1, 6.′′4, 6.′′5 and 12.′′0, respectively. WISE achieved 5σ point source sensitivitiesbetter than 0.08, 0.11, 1 and 6 mJy (corresponding to AB magnitudes of 19.1, 18.8,16.4 and 14.5; and to Vega-based magnitudes 16.5, 15.5, 11.2 and 7.9, respectively)in unconfused regions on the Ecliptic. The survey sensitivity improves toward theecliptic poles due to denser coverage and lower zodiacal background. Saturationaects photometry for sources brighter than approximately 8.0, 6.7, 3.8 and -0.4 mag(Vega) at 3.4, 4.6, 12 and 22 µm, respectively. The astrometric precision for highsignal-to-noise sources is better than 0.′′15.

The WISE All-Sky Release includes all data taken during the WISE full cryogenicmission phase (7 January 2010 to 6 August 2010): an Atlas of 18,240 images, aSource Catalog containing positional and photometric information for over 563 millionobjects, and an Explanatory Supplement.

Unlike IRAS catalogs which reported uxes in Jansky, WISE magnitudes arereported on the Vega magnitude scale. Although this dierence makes a direct com-parison with some IRAS-based studies more dicult, we follow already publishedwork based on WISE data and use unaltered cataloged Vega-based magnitudes.

2See http://wise2.ipac.caltech.edu/docs/release/allsky/

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0.0

0.2

0.4

0.6

0.8

1.0WISE

3.44.61222

0.0

0.2

0.4

0.6

0.8 IRAC3.64.55.88.0

0.0

0.2

0.4

0.6

0.8

rela

tive

spec

tral

resp

onse

func

tion

2MASS1.2351.6622.159

0.0

0.2

0.4

0.6

0.8 AKARIN2N3N4S7S9w

S11L15L18wL24

1 10 1000.0

0.2

0.4

0.6

0.8

wavelength [micron]

IRAS122560100

Figure 3.1: A comparison of bandpasses for WISE and other major infrared surveys.From top to bottom: WISE, IRAC, 2MASS, AKARI, IRAS.

3.2.2 Sample Selection

Wright et al. (2010) have demonstrated that WISE detected all the main familiesof extra-galactic sources: quasars (QSO) and various types of galaxies, includinggalaxies with active nuclei (AGN) and star-forming galaxies (SF). Their position in arepresentative WISE color-color diagram is schematically shown in the top panel inFigure 3.8. In order to enable a more quantitative comparison to our models, we usea subsample of WISE sources with SDSS-based identications.

We rst positionally matched WISE Preliminary Data Release and SDSS DataRelease 7 catalog using procedures described in Obri¢ et al. (2006) and Covey et al.(2007), with a matching radius of 1.5 arcsec. We classify a source as a star if it isunresolved in SDSS images, and as a galaxy if it is resolved. All matched sourcesthat are listed in SDSS catalog of quasars (Schneider et al., 2010) are classied asquasars. Galaxies with emission lines are further classied as star-forming and AGN

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galaxies using the Baldwin-Phillips-Terlevich diagram (Baldwin et al., 1981a) and se-lection boundaries from Obri¢ et al. (2006). The selected WISE-SDSS sample includes∼232,000 galaxies and ∼36,000 quasars.

When comparing model results to the observed source distribution in WISE color-color diagrams, we require that for each source the signal-to-noise ratio SNR > 10

in all four bands (this requirement roughly corresponds to a magnitude error < 0.1).For most sources, the most restrictive band is the 22 µm. Galaxies and quasarsare already ux-limited samples due to SDSS spectroscopic target selection criteria(approximately r < 18 and i < 19). For stars, we require that r < 20 and i < 19 toensure well-dened samples with precise SDSS photometry.

The quasars have the largest spread in redshift and the so-called K-correctionmust be taken into account when comparing data and models. Figure 3.2 shows thata nearly linear relationship exists between the observed WISE colors and redshiftup to z ≈ 1.5. We t a straight line using all quasars with z ≤ 1.5 and use thebest-t slope to estimate the K-correction. We nd that the eect of K-correction onthe mean quasar color is fairly small but not negligible (compared to the availablephotometric precision), with the correction most important for the [3.4]− [4.6] color.

0 1 2 3 4z

0.0

0.5

1.0

1.5

2.0

[3.4

] - [4

.6] i

n m

ags

slope = 0.41intercept = 0.93

0 1 2 3 4z

1.5

2.0

2.5

3.0

3.5

[12]

- [2

2] in

mag

s

slope = -0.01intercept = 2.40

0 1 2 3 4z

1.5

2.0

2.5

3.0

3.5

4.0

4.5

[4.6

] - [1

2] in

mag

s

slope = 0.14intercept = 2.81

0 1 2 3 4z

3.54.04.55.05.56.06.57.07.5

[4.6

] - [2

2] in

mag

sslope = 0.13

intercept = 5.220

100

200

300

400

500

QSO

/ bin

Figure 3.2: K-correction for quasars (QSO). The distribution of SDSS quasars withWISE detections as a function of redshift is shown for four WISE colors as scatterplots. Signal-to-noise ratio SNR > 10 was required in all four bands. A linear relationup to z ∼ 1.5 exists in all colors, and it is tightest in [3.4] − [4.6]. Linear ts to thedistributions are shown in red for QSOs with z ≤ 1.5 (1606 sources). If the scatter israther large (e.g. second panel from left), the resulting correction will be negligible.Note the dierent vertical scales in all panels. A histogram of all sources as a functionof z is shown in blue in the rightmost panel (only), with the right vertical axis of thatpanel showing the histogram scale.

Figure 3.3 shows two representative WISE color-magnitude diagrams for all se-lected sources grouped by the source class. In addition to the SNR and SDSS qualitycuts, in this gure we further require that stars must have [3.4] − [4.6] < 0.8. Thereason is that faint stars with [3.4] & 13 and [3.4]− [4.6] > 0.8 seem dominated byquasars (which are too faint to be listed in SDSS quasar catalog). Strong support forthis hypothesis is provided by their distribution in the SDSS g−r vs. u−g color-colordiagram shown in Figure 3.4. In addition, white dwarfs (WD) have similar colors inSDSS u − g color, but will in general not be confused with our faint objects since

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Table 3.1: Mean WISE colors of dierent source classes and Clumpy models

type→ Clumpy QSO* AGN SF Ellip Starsselected→ 1247400 1606 1910 6977 119 1400color↓[3.4]-[4.6] 1.43 0.93 (1.18) 0.60 0.29 0.38 -0.02[4.6]-[12] 3.95 2.82 (2.90) 3.33 3.96 3.71 0.26[12]-[22] 2.17 2.40 (2.40) 2.48 2.17 2.32 0.22[4.6]-[22] 6.11 5.22 (5.30) 5.81 6.13 6.03 0.48

(*) QSO colors before K-correction is applied are in parentheses.

WDs are bluer in SDSS g− r, as can for instance be seen from Fig. 23 in Ivezi¢ et al.(2007). Our nal sample sizes and their mean WISE colors are listed in Table 3.1.

9 10 11 12 13 14[3.4]

0.5

0.0

0.5

1.0

1.5

2.0

[3.4

] - [4

.6]

QSO (1606)

3 4 5 6 7[22]

1

0

1

2

3

4

[12]

- [2

2]

10 11 12 13 14[3.4]

AGN (1910)

4 5 6 7[22]

10 11 12 13 14[3.4]

SF galaxies (6977)

4 5 6 7[22]

10 11 12 13 14[3.4]

ellipticals (119)

4 5 6 7[22]

4 6 8 10 12 14[3.4]

stars (1400)

4 5 6 7 8[22]

Figure 3.3: Color-magnitude scatter plots for dierent classes of WISE sources. Classassignment is based on SDSS data. The following data quality and selection criteriawere applied: SNR > 10 in all four WISE bands for all sources, redshift z < 1.5 forQSOs, and SDSS magnitudes r < 20 and i < 19 for stars. In addition, [3.4]− [4.6] ≤0.8 and [3.4] ≤ 14 mag were enforced for stars (see Fig. 3.4 and text for motivation).The counts of selected sources are printed in parentheses above the top panels.

3.3 Model Results

Models produce spectral energy distributions (SED), which are then convolved withthe WISE bandpasses to produce model color-color tracks. These model tracks for agiven family of models are parametrized by the dust optical depth, with each familycorresponding to a given dust spatial distribution and chemical composition. Givenan SED, Fλ(λ), and the WISE bandpasses, Wf (λ), with f=3.4, 4.6, 12, and 22, the

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0 1 2 3SDSS u-g

0

1

2

SDSS

g-r

SDSS starsSDSS QSOsWISE faint "stars"

Figure 3.4: SDSS g-r vs. u-g color-color diagram. The distributions of stars andquasars are shown by contours (blue and red, respectively). The contour levels are0.1-0.9 in steps of 0.2. Objects that are unresolved in SDSS imaging data, and whichhave [3.4]−[4.6] > 0.8 and [3.4] ≤ 14 are shown as dots. All other selection criteria forstars as dened in Figure 3.3 were also applied. Most of these 218 objects are foundin the region occupied by quasars (e.q. see Figure 1 in Smol£i¢ et al. (2004), andare probably quasars that are too faint to be included in SDSS spectroscopic quasarsample. A signicant fraction of these objects are consistent with anomalously redquasars (found along and just above the stellar locus; for details, see Richards et al.2003).

in-band ux is computed as

Ff =

∫Wf (λ) · λFλ(λ) dλ∫

Wf (λ) · λF V egaλ (λ) dλ

(3.1)

Normalization is with the Vega ux according to Eq. 2 from Wright et al. (2010).The WISE colors are dened as [W1]− [W2] = 2.5 · lg(F2/F1).

The dust radiative transfer problem possesses general scaling properties, as dis-cussed in detail by Ivezi¢ and Elitzur (1997). For a given dust composition, there areonly two input quantities whose magnitudes matter: dust optical depth at some du-cial wavelength and the dust temperature at some point. All other input is denedby dimensionless, normalized proles that describe

1. the spectral shape of the external (input) radiation,

2. the spectral shape of the dust absorption and scattering coecients, and

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3. the dust spatial distribution.

Physical dimensions such as, e.g., luminosity and linear sizes are irrelevant. Scalingapplies to arbitrary geometries, and Ivezi¢ and Elitzur (1997) conducted extensivenumerical studies of its consequences for spherical shells. Dierent dusty objects are

expected to segregate in WISE color-color diagrams not because they have dierent

central sources, but rather because their dust shells are dierent .In addition to smooth spherical shells, we consider clumpy dust torus emission

models that are designed to explain infrared emission from quasars and AGNs.

3.3.1 Smooth Dusty Spherical Shells

Dusty spherical shells around a central source of radiation are a good model approx-imation for a large range of galactic sources, AGB stars in particular. We producedmodels of spherically symmetric dust distributions around a central source with ourpublicly available code dusty (Nenkova et al. 2000). dusty calculates exact so-lutions for the temperature proles, emerging uxes and other model properties ofinterest for a user-specied range of optical depths.

dusty utilizes the scaling properties of the radiative transfer problem. The onlydimensional parameters needed for the solution are the dust temperature at the innershell boundary and the shell overall optical depth at a given wavelength. All othermodel input is dimensionless: the spectral shape of the central source emission, thespectral shapes of dust absorption and scattering coecients, and the radial proleof dust distribution.

The spectral shape of the central source was taken as a black-body and outputwas produced for three model temperatures of Ts = 2, 500K, 5, 000K and 10, 000K.The source is embedded in a dusty spherical shell with a relative size of Y = 100,where Y = Rout/Rin is the ratio of outer to inner shell radius. We produced modelsfor a standard ISM mix and for typical dust found in AGB stars amorphous carbonfrom Hanner (1988) and warm silicates from Ossenkopf et al. (1992b). The grains areconsidered spherical with MRN size distribution (Mathis et al. 1977). The dust sizedistribution is approximated with a single-size composite dust grain by averaging overthe size distribution. This synthetic grain" approach is shown to produce results veryclose to the ones from exact treatment of grain mixtures (see for example Efstathiouand Rowan-Robinson 1994).

We calculated a range of models of dusty shells with overall optical depths at thevisual wavelength from τV = 0.1 to τV = 1, 000 and temperatures at the inner boundaryfrom Td = 600K to Td = 1, 400K. In our calculations we considered r−p dust densitydistributions (with p = 0, 1, 2) and the case of radiatively driven winds (RDW option,following Elitzur and Ivezi¢ 2001). Typical spectral energy distributions are shownin Figure 3.5 for a Y = 100 shell with τV = 100.

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amC

Oss-w

λ (μm)1 10 100

Extin

ctio

n Ef

ficie

ncy

10-3

10-2

10-1

100

101

p = 0

λ (μm)

1 10 100λfλ 10-4

10-3

10-2

10-1

100

p = 2

λ (μm)1 10 100

10-4

10-3

10-2

10-1

100

W1 W2 W3 W4

600K

Td = 1400K

600K

Td = 1400K

amC (dashed lines)Oss-w (full lines)

Figure 3.5: Top panel: extinction eciencies proles of the two types of model dustcompared to the WISE lters response functions; amC is for amorphous carbon andOss-w for Ossenkopf warm silicates. Bottom panels: sample SEDs for a central sourceat Ts = 10, 000K, and a Y = 100 dusty shell with an overall optical depth τV = 100.Results for two power law density proles are shown with p = 0, 2 and two modeldust temperatures at the inner boundary in each case.

3.3.1.1 Model Tracks for Smooth Spherical Distributions

The WISE color-color diagrams in Figure 3.6 show model tracks parametrized bythe shell optical depth. The black-body spectrum of the central source correspondsto τV = 0. The central source has Ts =104K, the shell relative size is Y = 100

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with two types of dust: Ossenkopf-warm silicates and amorphous carbon. The setof dust sublimation temperatures produces a family of closely spaced tracks fromTd = 600K (solid lines) to Td = 1, 400K (dash-dot lines). The data points on eachtrack correspond to optical depths of τV = 0.1, 1, 2, 5, 10, 20, 50, 100.

The separate panels show the results for r−p dust density distributions with p =

0, 1, 2. The results for radiatively driven winds are not shown in this gure as theyare practically identical to the p = 2 models.

Sil-Owp = 0

[4.6-12]0 2 4 6

0

1

2

3

4

5amC p = 0

[4.6-12]0 2 4 6amC

p = 1

[3.4-12]0 2 4 6

[3.4

-4.6

]

0

1

2

3

4

5

amC p = 2

0 2 4 6

0

1

2

3

4

5

Td = 600K

1200K

Td = 600K

1200K

[4.6-12]0 2 4 6

[3.4

] - [4

.6]

0

1

2

3

4

5

Sil-Ow p = 2

[4.6] - [12]0 2 4 6

0

1

2

3

4

5

100

1

10

Sil-Ow p = 1

1

100

0.1

2050

25

100

50

2021

0.1

1

100

5

1

100 Td=1400KTd=600K

τV=0

τV=0

τV=0

τV=0

τV=0

τV=0

100

[4.6-12]0 2 4 6

0

2

4

[4.6-12]0 2 4 6

[12]

- [2

2]

0

2

4

[4.6] - [12]0 2 4 6

0

2

4

Sil-Owp = 0

Sil-Owp = 1

Sil-Owp = 2

[4.6-12]0 2 4 6

[4.6-12]0 2 4 6

amC p = 0

amC p = 1

0 2 4 6

amCp = 2

1

100

1

Td=600K

100

Td=1400K

100

100

τV=0

τV=0τV=0

τV=0

τV=0 τV=0

100

1100

Figure 3.6: Model color-color tracks for spherical dusty shells around a central black-body source at Ts = 10, 000K. Each track begins at the color of the dust-free black-body. The optical depth increases along the tracks from τV = 0 to τV = 100, as shown.The dust is Ossenkopf-warm silicates (Oss-w) and amorphous carbon (amC) withtemperatures at the inner dust boundary Td = 600K (solid lines), Td = 1, 000K(dashed lines) and Td = 1, 400K (dash-dot lines).

As seen in Figure 3.6, a steeper density distribution (e.g., p = 2) produces anarrower distribution of tracks in the color-color diagrams compared to the at p = 0

prole. This is common for both dust types and it is to be expected. A steeper densityprole results in more dust closer to the heating source with dust temperature steeplyfalling across the shell and not very dierent for the two types of dust. Therefore, theobserved SED's for the two dust types show less of a dierence for the steep p = 2

prole compared to the at p = 0 prole, as seen in Figure 3.5.The [3.4] − [4.6] vs. [4.6] − [12] color plots are a useful tool for separating the

chemistry of circumstellar dust. As seen in the top panel of Figure 3.5, amorphous

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carbon absorbs more in the [3.4] and [4.6] bands, while silicates absorb more in the[12] and [22] bands. If two circumstellar shells have the same overall optical depth, thesilicate shell is expected to be redder in [4.6]− [12] color and bluer in the [3.4]− [4.6]

color. As a result, all model carbon tracks in the [3.4]− [4.6] vs. [4.6]− [12] plots areabove the silicate tracks for all density proles.

Based on the six panels on the left in Figure 3.6 one can predict that sources withpredominantly silicate dust and steeper density prole (e.g., typical AGB stars) canbe easily separated from such sources surrounded by carbonaceous dust (e.g., carbonstars) in [3.4]− [4.6] vs. [4.6]− [12] color plots.

The model tracks for carbon dust are almost degenerate with respect to the dusttemperature at the inner boundary for steep density distributions, while the corre-sponding tracks for silicates are more dispersed. This too can be explained by thesmoother extinction prole for amorphous carbon compared to the larger variationsfor silicates within the spectral ranges of the WISE lters.

The dust chemistry of circumstellar shells shows less of a distinction in the [4.6]−[12] vs. [12] − [22] plots. Silicate and carbon shells separate better only in the caseof steeper density proles and high optical depth. In that case the silicate shells areredder in [12] − [22] and bluer in the [4.6] − [12] color compared to the shells withamorphous carbon.

3.3.2 Clumpy Dusty Tori

In addition to the dusty models we have calculated the WISE colors for a largenumber of clumpy AGN dust torus emission models using our code Clumpy (Nenkovaet al., 2002, 2008a,b). These models employ a toroidal distribution of individuallyoptically thick dust clouds around a central, isotropic light source (the AGN). Thesingle cloud optical depth is specied by τavg, the average over orientations of aslab whose normal optical depth is τV at visual; the two are related via τavg = 2τV(Heymann et al., 2012). The radial torus extent Y = Ro/Rd is the ratio of its outerand inner radii, with silicate dust at 1500 K setting the dust sublimation radius Rd.The number of clouds per unit length in radial direction is distributed according toa power-law 1/rq, with q a free parameter. The average number of clouds along aradial ray in the equatorial plane is N0, and falls o for non-equatorial radial rayslike a Gaussian of width σ (measured in degrees from the equatorial plane). The nalfree parameter is the observer's viewing angle i on the torus, given in degrees fromthe torus axis.

Given the increased complexity of input parameters for clumpy torus model com-pared to spherical shells, instead of analyzing single model tracks parametrized byoptical depth, we generate a large number of models and study all of them simulta-neously. The sampled ranges of all parameters are given in Table 3.2. We computethe spectral energy distributions for 1.25 million combinations of the six free inputparameters. They are stored in a publicly accessible database3 and are also available

3www.pa.uky.edu/clumpy

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0

1

2

3

[3.4

] - [4

.6] i

n m

ag

galaxies w/o em. linesAGN galaxiesSDSS QSOsSF galaxiesstars

0 2 4 6[4.6] - [12] in mag

0

1

2

3

4

[12]

- [2

2] in

mag

0 2 4 6 8 10[4.6] - [22] in mag

0.0 0.5 1.0normalized CLUMPY model number density

Figure 3.7: A comparison of source distribution in WISE color-color diagrams andmodel predictions based on clumpy dust torus model. The distributions of stars andseveral types of extra-galactic sources are shown as contours (see inset for legend;the contour levels for all sources are 0.1-0.9 in steps of 0.2). The mean WISE colorsand the source counts for each type are given in Table 3.1. The normalized numberdensity histogram of ∼1.25 million Clumpy models is shown as gray scale map ona linear scale and normalized to peak density. These models are designed to explainthe colors of quasars (blue contours) and AGNs.

as an HDF5 le upon request.

3.3.2.1 Clumpy color-color diagrams for WISE

Figure 3.7 shows four WISE color-color diagrams, with the location of all ∼1.25million Clumpy models shown as a 2D number density histogram. Their locationcan be compared to the observed distributions of SDSS quasars and AGN galaxies.The highest density of Clumpy models aligns fairly well with the quasar location, andwith the red end of the distribution of AGN galaxies, for the [3.4]−[4.6] and [12]−[22]

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Table 3.2: Sampled Clumpy parameter values

Parameter Sampled Valuesq 0.0 - 3.0, in steps of 0.5N0 1 - 15, in steps of 1τavg 10, 20, 40, 60, 80, 120, 160, 200, 300Y 5, 10, 20, 30, 40, 50, 60, 70, 80, 90, 100σ 15 - 70, in steps of 5i 0 - 90, in steps of 10

Note: σ and i are measured in degrees.

-1 0 1 2 3 4 5 6 7[4.6] - [12] in mag

0

1

2

3

4

[3.4

] - [4

.6] i

n m

ag

τv =0.0 0.1 0.2 0.5 12

5

1020

50

100

200

100

DUSTY shellsp = 0 ISMp = 1p = 2p = 2 amC

0.0

0.5

1.0

norm

aliz

ed C

LUM

PY m

odel

num

ber d

ensi

ty

Figure 3.8: Comparison of models colors with WISE predictions. Left: Figure 12from Wright et al. (2010), reproduced by permission of the AAS and the authors.Right: The number density of Clumpy models is shown as a gray scale, normalizedto its peak value. For all models with a radial photon escape probability ≥ 50%the AGN power-law contribution was added to the SED before measuring the colors.Overplotted as solid lines are optical-depth-tracks for DUSTY spherical shell mod-els (with standard ISM dust), for three dierent exponents of the density law r−p

(with p = 0/1/2 shown in red/black/blue). The dashed line shows the same but foramorphous carbon dust with p = 2. The illuminating source is a blackbody withtemperature Ts = 5, 000K, and the dust temperature at the interface is Td = 1, 000K.

colors. The color osets of the models relative to quasars are 0.5 mag towards red,and 0.2 mag towards blue, respectively (using K-corrected quasar colors; the observedcolors are oset from models by 0.2 mag). The patch identied as "Seyferts" in Figure3.8 (top panel) falls on top of the region with the highest Clumpy model density inthe top left panel of Figure 3.7.

The model vs. data oset is the largest for the [4.6] − [12] color: models areredder than quasars by 1.1 mag. One possible explanation for this discrepancy that

44

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we have investigated is the impact of underlying AGN SED to the observed SED.However, it turns out that the input AGN spectrum does not contribute enough uxat wavelengths longer than 3.4 µm to explain the dierence.

The larger eect on the mean Clumpy model colors may lie elsewhere. From Moret al. (2009), Deo et al. (2011), and Nikutta et al. (2012, in prep.), we know that thecurrent Clumpy models probably under-estimate the amount of ux emerging in theK-band (∼ 2µm). This is most likely due to an insuciently accurate approximationof the complex dust sublimation zone of the torus (see above references for discussion).We note here that an addition of a single hot blackbody component which peaks inthe K-band would make the models bluer both in [3.4]− [4.6] and in [4.6]− [12], asrequired by WISE data. Another possibility for improvement is to model the dustsublimation zone more realistically using a mixture of dierent dust grain species.Work is under way in our group to achieve this.

3.3.2.2 Clumpy color-color diagrams for Spitzer

In addition to WISE colors we have calculated the colors of Clumpy models inSpitzer 's IRAC lters. Figure 3.9 shows a color-color diagram mimicking Fig. 1 fromStern et al. (2005). The gray scale shows, as a 2D-histogram, the number density ofClumpy models which fall into each small 2D-bin (normalized to unity).

The wedge outlined with red lines was identied by Stern et al. to empiricallyseparate active galaxies from normal galaxies and Galactic stars (see the selectioncriteria in their Section 4). It is encouraging to nd that 83% of our Clumpy modelslie within this "Stern-wedge" (i.e. within the region bounded by the red line andby the [3.6]-[4.5] = 1.5 line. 10% of all Clumpy models lie above the [3.6]-[4.5] =1.5 line, placing the remaining 7% to the red of the wedge in [5.8]-[8.0] visible in thegure.

Overplotted in blue are contour lines of the average 10-µm silicate feature strengthS10 per 2D-bin. The contour separation is in steps of 0.2 (see, e.g. Sirocky et al.(2008); Nikutta et al. (2009), for a denition of S10). Positive values of S10 mean asilicate feature is in emission, while negative values denote models with an absorptionfeature. Overall, models with colors in the vicinity of [3.6]-[4.5] ≈ 0.6 and [5.8-8.0]≈ 1.0 show the strongest 10-µm emission feature, while absorption is prevalent inmodels with [3.6]-[4.5] & 1.4.

Figure 3.10 shows the average values of Ptype1 (the probability to see the AGNdirectly) and f2 (the dust covering factor of the model) of all Clumpy models, inthe IRAC color-color space [3.6]-[4.5] vs. [5.8-8.0]. Note that Ptype1 depends onthe viewing angle, while f2 does not. These two quantities correlate strongly, sincein general a large covering factor increases the chances of encountering at least oneabsorbing cloud along radial lines of sight, and therefore of reducing Ptype1. It appearsthat models with the bluest colors (both in [3.6]-[4.5] and in [5.8]-[8.0]) tend to havethe largest probabilities to see the AGN (and thus to be identied as type-1 objects),and also the smallest dust covering factors.

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0 1 2 3[5.8] - [8.0] (Vega)

0

0.5

1

1.5

[3.6

] - [4

.5] (

Vega

)

0.8

0.6 0.4

0.4

0.4

0.2

0.2

0.0

-0.2

"Stern-wedge"contours of mean S10

0

0.5

1

mod

el d

ensi

ty (n

orm

aliz

ed)

Figure 3.9: Color-color diagram of all Clumpy models in Spitzer's IRAC colors [3.6]-[4.5] vs. [5.8]-[8.0]. The gray scale shows the density of models that fall into each small2D-bin of the color space (normalized to unity). The red lines conne a wedge-shapedarea which Stern et al. (2005) identied to empirically separate active galaxies fromnormal galaxies and Galactic stars (see their Figure 1). 83% of all Clumpy modelsare within these bounds. Overplotted in blue are the contour lines of the average10-µm silicate feature strength per 2D-bin. The separation of contour levels is 0.2.

3.4 Discussion and Conclusions

We have computed color-color tracks in WISE photometric system for two familiesof models: smooth spherical shells and clumpy dust torus models. With detectionsfor about 560 million objects, WISE represents a major step forward in the surveyingand understanding of the infrared sky. These model tracks provide guidance for theobserved distribution of sources in WISE color-color diagrams, such as illustratedin the top panel in Figure 3.8. The main results of our computations are shownin the bottom panel in Figure 3.8. As evident, the model-based color-color tracksoutline reasonably well the distribution of sources expected to be associated withdust emission (all source types except T dwarfs and stars without dusty shell).

Spherical dusty shell models are applicable to objects such as asymptotic giantbranch stars and various classes of young stellar objects. These simple models aresuccessful in explaining the overall color distribution of IRAS sources (Ivezi¢ andElitzur, 2000). In order to further investigate how well they describe WISE colors forsuch sources, samples of sucient size need to be constructed rst. Once they areavailable, it will be straightforward to perform model vs. data comparisons.

Clumpy dust torus models explained a variety of properties of infrared emission

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0 1 2 3[5.8] - [8.0] (Vega)

0

1

2

3

4[3

.6] -

[4.5

] (Ve

ga)

0 1 2 3[5.8] - [8.0] (Vega)

0 0.2 0.4 0.6 0.8 1avg. Ptype1

0.2 0.4 0.6 0.8 1avg. f2

Figure 3.10: Left: The average probability Ptype1 to the see the AGN directly, for allClumpy models in every small 2D-bin, in the color-color space of Spitzer's IRACcolors [3.6]-[4.5] vs. [5.8]-[8.0]. Right: Same, but with the color scale encoding theaverage dust covering factor f2 of all models in a 2D-bin.

from AGN and quasars (Nenkova et al., 2002, 2008a,b; Nikutta et al., 2009). Fig. 3.7shows that their colors align rather well the observed colors of QSOs and other AGN.In addition, Clumpy models agree very well with observations made with Spitzer,and most of them fall within the empirically determined "Stern-wedge" outlined inFig. 3.9. However, given new massive samples obtained by WISE, it is becomingincreasingly clear that moderate discrepancies between modeled and observed colorsare detected at statistically signicant levels. Furthermore, in order to model infraredemission from SF galaxies, and possibly from AGN galaxies as well, more sophisticatedmodels than presented here, such as dust layers with embedded sources, may berequired.

Therefore, the models presented here, while providing an overall approximate in-terpretation for the observed distribution of sources in WISE color-color diagrams, willneed to be signicantly improved to fully exploit the unprecedented WISE dataset.

3.5 Acknowledgments

We reproduced Figure 12 from Wright et al. (2010) as part of our Figure 3.8 bypermission of the AAS. We thank Chao-Wei Tsai for providing a high-quality versionto us.

This publication makes use of data products from the Wide-eld Infrared SurveyExplorer, which is a joint project of the University of California, Los Angeles, and theJet Propulsion Laboratory/California Institute of Technology, funded by the NationalAeronautics and Space Administration.

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Copyright c© Robert Nikutta 2012

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Chapter 4

The CLUMPY model database: Bayesian analysis and degeneracies

This chapter is in parts the preparation of a currently written paper, Nikutta, Asensio

Ramos, Thompson, Heymann, and Elitzur (2012, in prep.).

4.1 Introduction

The radiative transfer problem for heated dust is inherently degenerate (Vinkovi¢et al., 2003). Constraining the parameters is not possible from the spectral energydistribution (SED) alone, and high-resolution imaging is required. A toroidal andclumpy geometry introduces further ambiguities due to the relatively large numberof required parameters. Our formalism for radiative transfer in clumpy distributionsof dust around the central engines of active galactic nuclei (AGNs) was introduced inNenkova et al. (2002) and discussed in detail in Nenkova et al. (2008a) and Nenkovaet al. (2008b) (N02, N08a, N08b hereafter). Six free parameters fully describe thetorus. The only parameter related to a single cloud is τavg, its mean optical depth inthe visual band (0.55 µm). Four parameters describe the distribution of clouds withinthe torus. The radial distribution is modeled as a simple power law 1/rq, where r isthe distance from the AGN and q is a free parameter. The radial extent of the torusis Y . It is the ratio of the outer to inner torus radii, the inner radius being set tothe distance from the AGN at which dust sublimation occurs. While some authorshave modeled the maximal polar extent of the torus as a sharp edge, the availabledata do not support such a conguration (see, e.g., the related discussion and Fig. 3in N08b). We therefore model the angular distribution as a Gaussian-shaped gradualtransition, with on average N0 clouds along radial rays in the equatorial plane, andN(β) = N0 exp−β2/σ2 clouds along radial rays inclined by β from the equatorialplane. The angular width parameter of the torus, σ, is measured in degrees from theequatorial plane. Finally, the torus is observed at i degrees inclination from the torusaxis.

Our code Clumpy can generate SEDs for any combination of parameter values.A large database1 of torus models was calculated, and the sampling of Clumpyparameters for all results discussed in this work is listed in Table 4.1. The samplediers in comparison to the one used in Nikutta, Elitzur, and Lacy (2009) (NEL09hereafter) such that here we have left out values of N0 > 15, Y > 100 and σ > 70.They are physically rather unlikely, as was argued in, e.g., N08b. Overall nearly 1.25million Clumpy models were considered here.

1Publicly accessible at http://www.pa.uky.edu/clumpy/

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Table 4.1: Clumpy parameters used in tting

Parameter Sampled Valuesq 0, 0.5, 1, 1.5, 2, 2.5, 3N0 1 - 15τavg 10, 20, 40, 60, 80, 120, 160, 200, 300Y 5, 10, 20, 30, 40, 50, 60, 70, 80, 90, 100σ 15, 20, 25, 30, 35, 40, 45, 50, 55, 60, 65, 70i 0, 10, 20, 30, 40, 50, 60, 70, 80, 90

Note that σ and i are measured in degrees.

In addition to these changes, a recent update to the Clumpy formalism and DBneeds explanation. Deviating from Nenkova et al. (2002, 2008a,b) and all subsequentClumpy-related papers we have recently altered the denition of the optical depthof a single dust cloud. While previously τV was the optical depth of a dusty slabin a direction along the slab's normal, we came to realize from recent work in ourgroup (Heymann et al., 2012) that the optical depth of a cloud should be the depthof the slab, but averaged over all slab orientations. The new average optical depthis τavg = 2 τV (for the kind of "synthetic" clouds as we construct them). In practice,the change aects the photon escape probability Pesc in Clumpy (see Eq. (1.2),and also Fig. 2 in Nenkova et al. (2008b)). For any specic torus model this mayalter the spectral shape of the SED, and especially of the silicate features at 10µm

and 18µm. We tested the eect of the new denition on the ensemble of models,and found that many ensemble quantities were not much aected by the new opticaldepth denition, for instance the distributions of WISE photometric colors for all 1.25million Clumpy models, and the histograms of the 10µm silicate feature strength S10.A detailed comparison will be published elsewhere.

4.2 Fitting of SEDs

If a model predicts values mj when compared (i.e. "t") to an observed datasetdj at Nwav wavelengths j, it achieves a goodness-of-t measure

χ2 =Nwav∑j=1

(mj − djσj

)2

, (4.1)

where σj are the one-sigma errors on the observed data points. Dividing by thenumber of degrees of freedom, Ndof = Nwav − Nfree, we obtain the "reduced chisquared" measure

χ2r = χ2/Ndof . (4.2)

Nfree is the number of free parameters in the model. It is 6 for the Clumpy torusmodel (Section 4.1), and 7 or more if additional SED components are added during

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the tting (see Section 4.3). An observed SED comprises the uxes dj = λjFoj at a

set of Nwav wavelengths λj. To t the data with the Clumpy torus models the modeloutputs are provided as synthetic uxes

mj = λFλ/FAGN . (4.3)

Since dust radiative transfer solutions are self-similar (Ivezi¢ and Elitzur, 1997) themodel SED can (and must) be scaled by a factor FAGN calculated such that χ2

r isminimized. This scale also determines the bolometric ux of the model.

Fitting an SED means to nd the model SED that provides the overall smallestχ2r among the family of many realizations of this model, each with dierent model

parameter values.

4.3 Multi-component SEDs

The observed IR-SEDs of AGN often comprise not only light from the torus itself,but also contain other components. Due to their large distance from Earth, even withvery large telescopes it might be impossible to resolve only the torus. Then the eldof view is contaminated by radiation that is not originating from the dusty torus, butfrom other sources at a greater distance from the AGN.

4.3.1 Addition of a blackbody component to torus SEDs

Many luminous type 1 AGN show an excess of ux in the near-infrared (NIR), typi-cally peaking locally around ∼1-5 µm. Such spectral bumps have been reported andinvestigated both for individual sources and for samples of quasars (e.g., Barvainis,1987; Pier and Krolik, 1993; Riel et al., 2009; Gallagher et al., 2007; Netzer et al.,2007; Mor et al., 2009; Leipski et al., 2010). The shape of the NIR emission couldoften be modeled with a single Planck function of temperature typically close to thedust sublimation. In the case of PG quasars Pier and Krolik (1993) tried to accountfor the additional radiation by including a 1300 K hot blackbody (BB) componentin their ts to the data. With the availability of better data from Spitzer Mor et al.(2009) have recently picked up on this idea and also included a hot BB component intheir three-component (BB + Clumpy torus + narrow line region) ts to the data ofPG quasars. They found that by adding the BB component their overall ts could begreatly improved. While Pier and Krolik held the temperature xed at 1300 K andallowed the scale of the BB to change, Mor et al. varied both the temperature andthe scale. We will show that given the observational data the optimal scale of theBB component can be calculated analytically, and only its temperature TBB must beallowed to vary. The optimal temperature is found by minimizing χ2(TBB).

Deo et al. (2011) nd such an excess of NIR radiation also in many other quasars.Its origin is not yet entirely clear. Radiation from an old stellar population near thegalactic center as well as starburst activity in the host galaxies have been ruled outon general grounds by Mor et al. (2009). They have also noted that the emission

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can not be produced by even hotter clouds of dust that have the same chemicalcomposition as the dust producing the 10µm and 18µm silicate features, because thiswould signicantly alter the features' strengths and shapes. If it is indeed a regionof the torus that produces the signature of a hot BB in the SED, it must be lledwith dust and located close to the AGN. Our current Clumpy modeling involves asharp transition between the dust-free inner cavity of the torus and the dust-lledregions; this transition occurs at the sublimation temperature of the dust, in ourcase 1500 K for the silicate-graphite composite grain. In reality, however, there willbe multiple dust species present of dierent chemical compositions and grain sizedistributions. Larger grains will survive closer to the AGN, as will species richer ingraphite. Therefore the inner edge of the dust torus will be a smooth and somewhatextended transitional region rather than a sharp boundary. This is the most likelyorigin of a hot BB component that in the SEDs typically peaks between 1 and 5µm. Proper physical modeling of a multiple-grain dust sublimation region is underway in our group and the results will be published elsewhere. In the meantime wehave implemented the option of adding a BB component to every individual ttedClumpy model, yielding the two-component model uxes

Mj = B · bj + T · tj = Bj + Tj, (4.4)

with B and T the optimal scales of the BB and the torus, respectively. The spectralshapes of the torus and BB components, tj and bj, are normalized to unit area.Replacing the model uxes FAGN · mj in Eq. (4.3) with Eq. (4.4) gives a multi-component expression for χ2

χ2 =Nwav∑j=1

(B · bj + T · tj − dj

σj

)2

. (4.5)

Given a set of data, the optimal scales can be calculated analytically (see Section Afor a derivation of the procedure). Therefore the inclusion of a BB component requiresonly one additional free parameter the BB's temperature TBB. The temperaturefully denes the spectral shape of a blackbody. We usually set the range of permittedtemperatures to 8001800 K, corresponding to BB emission peaks between 3.6µm

and 1.6µm, respectively (via Wien's displacement law). 1800K is also the sublimationtemperature of pure graphite.

In many cases the tting error can be greatly reduced in comparison to a torus-only t. In Deo et al. (2011) we t the UV and IR data (from SDSS and Spitzer,respectively) for 25 type-1 SDSS quasars, all with redshifts between 1.62.2. The χ2

r

values for all sources experienced an improvement by a factor of 3.2 on average, andeven by up to 13.8 in some cases. For these 25 quasars Figure 4.1 shows the best-tobtained with the two tting attempts: torus+blackbody composite model (black),and Clumpy torus only (blue). The models are plotted on top of the data, which isshown in gray with error bars. The composite models are a great improvement overany single-component t. The reason for this improvement is mainly that the BB

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10-16

10-15

10-14

λFλ

[Wm−

2]

095047.47+480047.3

original datafitted datatorus onlytorus+blackbody

100401.27+423123.0 103931.14+581709.4 104114.48+575023.9 104155.16+571603.0

10-16

10-15

10-14

λFλ

[Wm−

2]

104355.49+562757.1 105001.04+591111.9 105153.77+565005.7 105447.28+581909.5 105951.05+090905.7

10-16

10-15

10-14

λFλ

[Wm−

2]

132120.48+574259.4 142730.19+324106.4 142954.70+330134.7 143102.94+323927.8 143605.07+334242.6

10-16

10-15

10-14

λFλ

[Wm−

2]

151307.75+605956.9 160004.33+550429.9 160950.72+532909.5 161007.11+535814.0 161238.27+532255.0

0.1 1 10λ [µm]

10-16

10-15

10-14

λFλ

[Wm−

2]

163021.65+411147.1

0.1 1 10λ [µm]

163425.11+404152.4

0.1 1 10λ [µm]

163952.85+410344.8

0.1 1 10λ [µm]

164016.08+412101.2

0.1 1 10λ [µm]

172522.06+595251.0

Figure 4.1: Best ts to UV+IR SEDs of 25 type-1 quasars (see Deo et al., 2011),using a Clumpy torus-only model (blue), or a composite torus + blackbody model(black). The data are shown with error bars.

component can provide the bulk of ux in the NIR, while the torus can reproduce thesilicate feature regions with greater delity. The freedom of an additional parameterenables torus models to perform much better that were previously deemed to be a badt; note that when an additional SED component is introduced (here the BB), theprevious component (here the torus) may assume quite dierent parameter values.Only the multi-component SED as a whole needs to minimize χ2

r, not the individualcomponents alone.

Depending on the exact shape of the spectral data, evaluation of the optimalblackbody and torus scales B and T can yield a mathematically correct solution withone of the components having a negative scale (see Appendix A for more discussion).This of course is not a physically meaningful solution, and in such cases we set B tozero. The addition of a BB component to the torus did not improve the t qualityfor that particular model, and we revert to a torus-only t.

The relative importance of the added BB component varies among tted objects.We calculate the overall contribution of the BB component to the composite model

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in the IR spanning 1100 µm through

fBB =

100µm∫1µm

FBBλ dλ /

100µm∫1µm

F torus+BBλ dλ. (4.6)

The torus contribution is the complement ftorus = 1− fBB. For the sources we ttedin Deo et al. (2011) the BB fraction fBB varies between ≈ 10% and ≈ 50% for mostsources, with an average of 33%.

4.3.2 Over-tting

The freedom of having multiple SED components available in tting any particularobservational data adds free parameters to the composite model. This generallyimproves the "exibility" of the tted model, such that it can easier adapt to t thedata, although neither of the individual SED components would t the dataset wellby itself.

While often this is desirable, or even unavoidable, one must make sure that thereis evidence in support of the decision to introduce ever more free parameters to themodel. Otherwise, if not careful, one may be led to believe that a model generatesa wonderful t to the data, while in fact all it is doing is over-tting the data withunjustied model complexity. We show in Figure 4.2 one example. Mid-IR Spitzerdata of NGC5506 (shown in gray with error bars) are being modeled four times (thefour panels of the gure), each time increasing the model complexity. In the toppanel a search for a best-t model in the Clumpy database of torus-only models wasperformed. Even the formally best-t torus model (shown as a black solid line) is amiserable t to the data. It fails to reproduce both the spectral shape of the 10µm

silicate feature and the overall slope of the SED. Evidently, the torus-only model isnot the right physical explanation for the source of the observed SED. The χ2

r valuefor the best model is 4.00.

For the modeling shown in the second panel from the top another degree of freedomwas added to the torus model: a global extinction law exp−A · τλ with which thetorus SED is multiplied. A is the new free parameter and determines the strengthof the extinction. The spectral shape of the extinction law is determined by τλ, thespectral dependence of the dust extinction coecient. The second panel in Figure4.2 shows again the data, and the best-t torus model (with extinction applied) inblack. This time the 10µm silicate feature is reproduced much better by the model,and also the overall shape of the model SED is closer to that of the observed SED.Where the model still fails though is at the blue end of wavelength range, shortwardof ∼ 8µm. The χ2

r value for this model is 1.73.Pushing the model further, panels 3 and 4 show the result of tting with and

without a dust extinction applied (just like panels 1 and 2), but with the addition ofa separate blackbody component to the model SED. The BB in the best-t compositemodels is shown in red, the torus in green, and the sum of both in black. Without

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10-2 10-1 100 101 102 103wavelength [µm]

10-14

10-13

10-12

λFλ[W

/m

2]

zoom

i = 89.99τv = 20.00q = 0.45N0 = 14.00σ = 70.00Y = 90.00χ2 = 1314.649χ 2r = 3.996 data

MAP model

101wavelength [µm]

10-13

2e+04

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ple

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r

best fit = 89.99median = 84.001σ interval = [77.2,88.2]2σ interval = [68.2,89.7]

location of best fitmedian1σ credible interval (= 68.3%)2σ credible interval (= 95.4%)

25 50 75 100 125τv

best fit = 20.00median = 16.641σ interval = [13.3,20.3]2σ interval = [10.8,22.8]

0.5 1.0 1.5 2.0 2.5q

best fit = 0.45median = 0.401σ interval = [0.4,0.4]2σ interval = [0.3,0.5]

2.5 5.0 7.5 10.0 12.5N0

best fit = 14.00median = 14.301σ interval = [13.7,14.8]2σ interval = [13.1,15.0]

20 30 40 50 60σ

best fit = 70.00median = 68.621σ interval = [67.6,69.6]2σ interval = [66.8,69.9]

20 40 60 80 100Y

best fit = 90.00median = 89.141σ interval = [82.3,96.0]2σ interval = [77.5,99.4]

NGC5506_nolines_weighted.txt_fakeYq

10-2 10-1 100 101 102 103wavelength [µm]

10-14

10-13

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λFλ[W

/m2]

zoom

i = 89.97τv = 5.00q = 1.03N0 = 5.90σ = 69.99Y = 35.97Av = 34.47χ2 = 568.618χ 2r = 1.734 data

MAP model

101wavelength [µm]

10-13

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best fit = 89.97median = 55.671σ interval = [18.6,81.0]2σ interval = [3.8,88.8]

location of best fitmedian1σ credible interval (= 68.3%)2σ credible interval (= 95.4%)

25 50 75 100 125τv

best fit = 5.00median = 6.411σ interval = [5.4,7.9]2σ interval = [5.0,9.1]

0.5 1.0 1.5 2.0 2.5q

best fit = 1.03median = 1.161σ interval = [1.0,1.3]2σ interval = [0.9,1.4]

2.5 5.0 7.5 10.0 12.5N0

best fit = 5.90median = 5.721σ interval = [5.2,6.3]2σ interval = [4.6,6.9]

20 30 40 50 60σ

best fit = 69.99median = 65.441σ interval = [59.3,68.7]2σ interval = [51.1,69.8]

20 40 60 80Y

best fit = 35.97median = 32.181σ interval = [28.7,34.6]2σ interval = [25.4,37.0]

10 20 30 40 50Av

best fit = 34.47median = 33.631σ interval = [31.7,35.7]2σ interval = [29.8,38.1]

NGC5506_nolines_weighted.txt_fakeYq

10-2 10-1 100 101 102 103wavelength [µm]

10-14

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zoom

i = 64.08τv = 20.00q = 0.59N0 = 12.00σ = 70.00Y = 14.96Tbb = 1500.00χ2 = 138.033χ 2r = 0.421

datacomponent 0component 1MAP model

101wavelength [µm]

10-13

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best fit = 64.08median = 65.461σ interval = [51.7,81.1]2σ interval = [42.1,88.6]

location of best fitmedian1σ credible interval (= 68.3%)2σ credible interval (= 95.4%)

25 50 75 100 125τv

best fit = 20.00median = 17.751σ interval = [14.1,20.9]2σ interval = [11.4,23.1]

0.5 1.0 1.5 2.0 2.5q

best fit = 0.59median = 0.551σ interval = [0.3,0.8]2σ interval = [0.1,0.9]

2.5 5.0 7.5 10.0 12.5N0

best fit = 12.00median = 12.561σ interval = [10.9,14.2]2σ interval = [9.7,14.9]

20 30 40 50 60σ

best fit = 70.00median = 67.491σ interval = [64.4,69.2]2σ interval = [60.6,69.9]

20 40 60 80Y

best fit = 14.96median = 14.031σ interval = [11.8,15.8]2σ interval = [9.6,17.3]

600 800 1000 1200 1400Tbb

best fit = 1500.00median = 1464.001σ interval = [1424.5,1488.6]2σ interval = [1366.8,1498.4]

NGC5506_nolines_weighted.txt_fakeYq

10-2 10-1 100 101 102 103wavelength [µm]

10-14

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/m2]

zoom

i = 90.00τv = 150.00q = 0.00N0 = 15.00σ = 70.00Y = 7.31Tbb = 1180.53Av = 22.00χ2 = 103.436χ 2r = 0.316

datacomponent 0component 1MAP model

101wavelength [µm]

10-13

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best fit = 90.00median = 75.851σ interval = [57.5,86.0]2σ interval = [31.9,89.4]

location of best fitmedian1σ credible interval (= 68.3%)2σ credible interval (= 95.4%)

25 50 75 100 125τv

best fit = 150.00median = 144.201σ interval = [136.9,148.2]2σ interval = [125.0,149.7]

0.5 1.0 1.5 2.0 2.5q

best fit = 0.00median = 0.351σ interval = [0.1,0.7]2σ interval = [0.0,0.9]

2.5 5.0 7.5 10.0 12.5N0

best fit = 15.00median = 12.991σ interval = [10.5,14.5]2σ interval = [7.8,14.9]

20 30 40 50 60σ

best fit = 70.00median = 62.151σ interval = [53.3,67.8]2σ interval = [44.4,69.7]

20 40 60 80Y

best fit = 7.31median = 6.341σ interval = [5.4,8.0]2σ interval = [5.0,10.1]

600 800 1000 1200 1400Tbb

best fit = 1180.53median = 1231.071σ interval = [1145.9,1335.7]2σ interval = [1077.1,1446.6]

10 20 30 40 50Av

best fit = 22.00median = 20.381σ interval = [19.0,21.8]2σ interval = [17.5,23.0]

NGC5506_nolines_weighted.txt_fakeYq

Figure 4.2: From top to bottom, the same Spitzer SED of NGC5506 (shown in graywith error bars) is t with models of increasing complexity. Panel 1: best torus-onlyt, with χ2

r = 4.00. Panel 2: The strength of dust extinction was added as a freeparameter to the torus-only model. Best χ2

r = 1.73. Panel 3: like panel 1, butwith the addition of a blackbody (red) component to the torus (green) SED. Thebest composite model (black) has χ2

r = 0.42. Panel 4: BB+torus model, plus dustextinction parameter. The best χ2

r = 0.32.

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extinction (panel 3), the composite model already amends the shortcomings of bothBB-free models discussed before, and the short-wavelength data is now matched well.The χ2

r value for this best-t model is 0.42. Combining both the dust extinctionfree parameter and the BB component in the SED, the most-complex model (panel4) unsurprisingly reproduces the data most faithfully. The χ2

r value for the bestcomposite model SED is 0.32.

Whether the most complex model is to be preferred can not be decided only bythe given data. The BB component peaks at wavelengths that are not covered bythe data, so only the Rayleigh-Jeans tail of the BB function is being used for tting.This tail has identical slope in all blackbodies, meaning that the BB temperature (afree parameter of the model!) is meaningless. Any blackbody will do the job equallywell as long as its peak is outside of the tted wavelength range.

In Section 4.4.10 I will describe a formal method for theory selection that balancesbetween desired tting power and required complexity.

4.4 Bayesian inference

The χ2r value of an individual model measures the overall goodness of t of that

particular model to the data. The parameter values associated with that model donot tell how likely they are, among all possible parameter values, to t the data.Calculating χ2

r for all the models in the database provides more powerful meansof analysis. The model with minimal χ2

r is considered the best t. To study thedistributions of parameters values of models close in χ2

r-space to the best-t model,NEL09 have presented an approach, and it has since then been applied in other works(Deo et al. (2011), Malmrose et al. (2011b)). The method, however, constrains onlyone parameter at a time, and is generally unable to condently restrict an entire ttedmodel. In fact, the full parameter probability function, or posterior distribution, issix-dimensional (seven-dimensional, if the BB component is added to the tting, andeven 8-dimensional if dust extinction is a free parameter also), and it is impossible torepresent it graphically. Clearly, a more holistic approach to the problem is needed,and it exists in the form of Bayesian analysis.

4.4.1 Bayes' Theorem

The values mi of the model output are of course a function of the model's parameters,and we can write mi = f(θ), with θ = q,N0, τavg, Y, σ, i the parameter vector(here 6 parameters for the Clumpy torus model). The most interesting questionwhen tting an entire database of models to some data is to answer what ranges ofparameter values are most likely to deliver good ts, and to quantify the degree ofcondence one can have in such estimates. Bayes' Theorem gives the simple yet verypowerful prescription on how to achieve the goal

P (θ|D) =P (θ)

P (D)P (D|θ). (4.7)

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The left-hand side of the equation denotes the full posterior of the parameters θ, inlight of the data D. This is a probability distribution, and a function of θ. Theposterior is also called inverse probability, because if allows to compute the answerto an inverted problem: knowing only about the data, and having no knowledge ofthe true parameter value distributions, what is the probability that the parameterstting the data best will have certain values?

The posterior is calculated as a product of the so-called prior P (θ) and the likeli-hood P (D|θ), normalized by a constant P (D) (called the evidence). The prior (usu-ally) does not depend on the data, and only expresses the probability distribution ofparameter values (or bias) before even having introduced the data to the problem. Inthe case of our Clumpy torus for instance the prior is often uniform, or "at", overthe parameter ranges.

The evidence, for the purpose of parameter inference, is irrelevant. It is only anormalization constant, and for most practical problems is also rather dicult tocompute. This is however not necessary, as the obtained posterior can be simply re-normalized after the calculations such that it fullls the requirements of a probabilitydensity. We will therefore simplify Eq. (4.7) to

P (θ|D) ∝ P (θ) · P (D|θ). (4.8)

4.4.2 Likelihood

Having established that the prior P (θ) is a probability distribution of parametervalues known beforehand, all that remains to be done is to compute the likelihood termP (D|θ) in Eq. (4.8). It is the likelihood that a particular set of parameters θ generatesa model SED compatible with the data D. The observed data uxes di obtainedwith some instrument carry intrinsic errors σi. They originate both from the noisyinstruments (e.g. thermal CCD noise, read-out noise, noisy amplier electronics, etc.),and from observational eects such as low signal-to-noise ratio, uneven illuminationof the recording CCD, etc. The entirety of all sources of error/noise can be oftenestimated as a Gaussian of given width σ. Given a (Gauss-)noisy data ux point djthe individual probability of a modeled ux point mj being compatible with the datais

P (dj|θ) = e− (mj − dj)2/(2σ2j ). (4.9)

If a set of parameter values generated a model SED that exactly reproduced thej-th data point (mj = dj), this probability would be 1. Strictly speaking P (dj|θ)

is a probability density, but since we can ignore the absolute normalizing constant,we use the terms equivalently. Assuming that all data channels are independent (areasonable rst-order assumption), the probability or likelihood of the entire modeledset mj being compatible with the set of data points D = dj follows from themultiplication rule for independent events

P (D|θ) =Nwav∏i=j

P (dj|θ) =Nwav∏i=j

exp− (mj − dj)2/(2σ2j )

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= exp

Nwav∑i=j

(mj − dj)2/(2σ2j )

= exp−χ2/2. (via Eq. (4.1))

(4.10)

Since our priors P (θ) are uniform and the evidence P (D) is a constant, Bayes' theoremreduces to

P (θ|D) = C · P (D|θ), (4.11)

i.e. the posterior is simply proportional to the likelihood of the parameters, withsome normalizing constant C.

4.4.3 Marginalized posteriors

The full multi-dimensional posterior is of limited use in typical modeling scenarios,and one will be more interested in obtaining the one-dimensional posterior probabilitydistributions for each of the Npar parameters θk ∈ θ, k ∈ 1 . . . Npar. These so-called marginalized posteriors are calculated by integrating the full posterior over allparameters but the one in question

P (θk|D) =

∫dθ1dθ2 . . . dθk−1dθk+1 . . . dθNparP (θ|D). (4.12)

4.4.4 Markov chain Monte Carlo

If we now were in possession of an analytical expression for the likelihood as a functionof θ and D, we could proceed and calculate the full and the marginalized posteriorsdirectly (since the priors are known analytically). Unfortunately, such an expressiondoes not exist in most practical cases. We thus need to sample the full space ofparameter values, each time computing the output of the model given the sampledparameter values, then measuring how well a model with these parameters ts thedata, and then somehow combining the results in Bayes' Theorem to compute theposterior.

Wanting to sample the a-priori (and per denition) unknown full posterior of amodel (in our case 6-dimensional) several techniques come to mind that were devel-oped with the advent of ever faster hardware. Among those, Markov chain Monte

Carlo (MCMC) methods, and especially the Metropolis-Hastings family of samplingalgorithms (Metropolis et al., 1953; Hastings, 1970), have become most popular inthe scientic community. Another popular and powerful method is nested sampling

(Skilling, 2004).What is meant by "a model"? A model is simply a prescription (or a formula for

instance) on how to calculate the output of a process, when fed with any combinationof parameter values. As a toy example we can imagine trying to t a set of y(x)

data which we believe is scattered randomly around a straight line. The bottom rightpanel in Figure 4.3 shows such data with black dots and error bars. If we now imagine

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0 20000 40000 60000 80000 100000iteration

1.8

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sample size = 1.0e+05

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0 50 100 150 200 250x

200

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data and fitted line; y = 2.231 * x + 35.044

MAP

mean

Figure 4.3: Example of MCMC sampling. A set of y(x) data (bottom right panel)with y-error bars is to be modeled with a straight line y(x) = mx + b, with m andb free parameters. The Markov chains (105 samples long) for both parameters areshown as a trace in the upper panels (the green portion of the trace is the burn-inphase). The histograms of the traces, shown in the middle panels, are the posteriorsof the parameters. The bottom left panel shows a 2d-histogram of the Markov chain.Its integration along each of the axes would produce the 1d-histograms. The redline in the bottom right panel represents the model with m, b values taken from themedian of each marginalized posterior. The dashed line is the MAP model (see text).

that the data might be following a linear relation, then y(x|m, b) = mx + b is ourmodel. It predicts what the values of y (the output) should be, given the values ofthe models' two free parameters: the slope m and intercept b of the straight line.Parameter inference is then a method of nding those values of m and b for whichthe model delivers a minimal χ2.

For our toy example, and in fact further below for sampling the Clumpy database,I use the PyMC2 package for Python, which, as the name suggests, oers MCMCsampling methods that can be sub-classed in Python and can also be easily adapted toany specic science problem. PyMC shines in its ease of use: setting up a model withthe to-be-sampled parameters, instantiating a sampler, and performing the sampling,can be achieved in just a few lines of code.

2https://github.com/pymc-devs/pymc

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PyMC (and any other sampling tool such as, e.g., Win/OpenBUGS Lunn et al. (2009)or emcee Foreman-Mackey et al. (2012)) allows to dene permissible ranges for the freeparameters, and then to run Markov chain sampling for the duration of a pre-denednumber of drawn samples. At each step the tool will draw randomly (according toa proposal distribution) a 2d-location in the space of parameters, then compute theoutput of the model given these parameter values, calculate a measure for the good-ness of t of this particular output, and then proceed with the next sample. Followingthe Metropolis-Hastings algorithm, an MCMC sample will make a judgment aboutwhere in the parameter space to jump to next. Whenever the newly drawn samplecauses the model likelihood to increase, the algorithm will accept this sample andjump to the new location. However, if the new sample worsens the t (i.e. decreasesthe currently held likelihood), the algorithm will sometimes reject it, and sometimesaccept it. The probability of rejection is proportional to how big the gap betweenthe likelihoods at the current and the new locations is. In the original MCMC papersit has been shown that the Markov chain then asymptotically converges towards anequilibrium distribution. After achieving equilibrium, the Markov chain from thenon only returns values according to a probability density distribution that resemblesthe sought-after posterior distribution.

In our toy example of tting a straight line to scattered y(x) data the lists, ortraces, of all sampled values (105 samples) in the two-dimensional parameter space(slopem and intercept b of the straight line) are shown as a function of sample numberin the two top panels of Figure 4.3. After an initial run of discarded samples (the burn-in phase, during which the Markov chain converges to an equilibrium distribution),the traces display a stable behavior, and a sub-range of each parameter's entire rangeof values is being sampled. This can be seen better in the histograms of the traces(the middle row of panels in the gure.). By denition of a Markov chain that hasconverged toward an equilibrium, the histograms are the posteriors of the modelparameters. They include both the knowledge of any priors being imposed on theparameters before seeing the data, and the eect of exposing the models to the data.The modes or medians of the histograms can be used to characterize the posteriorswith just one number, but the true answer to a Bayesian parameter inference problemis the full posterior. It is therefore better to for instance always give the median andthe 1σ-range around it.

These condence intervals, or in Bayesian context credible intervals3, express aquantitative level of trust in the obtained results, much more meaningful than a singlebest-t model ever could. Since the posteriors are probability density functions, it issimple to calculate the credible intervals. Deriving from a normal distribution, theyare those ranges on the parameter axes around the median that contain 68.3% (1σ-level) or 95.4% (1σ) of the total area under the posterior curve. One must thus nd

3The two are not entirely equivalent. In Bayesian statistics the credible intervals incorporateinformation about the prior parameter distributions, which the frequentist condence intervals donot deal with at all. In addition, the treatment of so-called nuisance parameters is very dierent inboth approaches.

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the parameter values for which the cumulative distribution function (CDF) reaches0.159 and 0.841 for the 1σ-level, or 0.023 and 0.977 for the 2σ-level.

The bottom left panel of Figure 4.3 shows a two-dimensional histogram of thedistribution of drawn samples in the space of parameter values m and b. In just twodimensions such a plot can be made, and can be very instructive. The integrationof this 2d-histogram onto each of the two axes would produce the histograms in themiddle panels. They are thus the marginalized posteriors (see Section 4.4.3).

Finally, the red line in the bottom right panel represents the model with m, b

values taken from the medians of each marginalized posterior. The dashed line inthe same panel is the model with parameter values dened such that they together

maximize the product of prior and likelihood (since our priors are at, the parametervalues maximize the likelihood). This is often referred to as the MAP model, formaximum-a-posteriori.

4.4.5 Interpolation of the database

The discretely sampled parameters in the Clumpy model database should not leadthe reader to believe that the parameters themselves are discrete. Of course, in thereal physical world the quantities expressed by the model parameters are continuous(even N0, the number of discrete clouds per radial equatorial ray, is continuous, sinceN0 is the mean of a Poissonian, and thus can be fractional). The problem of discreteparameter sampling arises only from a practical point of view: since the computationof a single Clumpy model requires time in the order of 0.55 minutes, it is notfeasible to compute the models "on the y" when sampling the parameter space. OurClumpy database therefore stores the model output (the synthetic torus SEDs) at1.25 million pre-sampled parameter locations (each a 6-d tuple) for later use. Ideally,however, it would be desirable to have truly continuous parameter spaces. This is,in most real-world scenarios, far from possible. However, we are condent that nounexpected behavior of the model output was missed between the sampled parametervalues. The reason is that the model output (the SEDs) changes smoothly withthe input parameter values, and we have convincing empirical indications that no"spiky" behavior ever occurs given the dense initial sampling in out model database.We can thus set out to interpolate the model output between the sampled parameterswherever required.

4.4.5.1 Interpolation by Articial Neural Network

Asensio Ramos and Ramos Almeida (2009) made a rst such attempt at interpolatingthe Clumpy database in their tool BayesCLUMPY by training an Articial NeuralNetwork (ANN) with a sub-sample of the Clumpy DB. First however, the authorscarried out a principal component analysis (PCA) to reduce the computing time formodel interpolation. We have revisited their approach and examined the techniquein detail. The use of PCA reduces the dimensionality of the model database through

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Figure 4.4: Comparison of an original Clumpy model SED (black) with its ANN-reproduced version (red). The horizontal axis is wavelength (in µm), and the verticalis ux (in arbitrary units). This particular model is the one that suers the worstreproduction of all models in the DB. Figure courtesy of Grant Thompson (priv.comm.)

describing each model not by all initial 125 data points, but rather by several principalcomponents or eigenvectors. As Asensio Ramos and Ramos Almeida nd, a fewcomponents are sucient to successfully reproduce all models, thus reducing boththe size of the database and the computational time. We conrm that 12 PCAeigenvectors suciently reproduce the model database within 1% accuracy.

The subsequent "training" means that the ANN tried to learn, in a highly non-linear fashion, the mapping between model parameters and projections along thePCA eigenvectors (the SEDs reduced in complexity). Once complete, the learnedmapping could be used to interpolate the model SEDs at parameter vertices whichhave previously not been stored in the DB. This approach was a major step forward inunderstanding how to explore the Clumpy database in its entirety, and it was appliedto observations in several papers (e.g.: Ramos Almeida et al., 2009; Alonso-Herreroet al., 2011).

The ANN mapping, however, did introduce new (and uncontrolled) uncertaintiesto the space of SEDs used for tting. We nd that for more than 90% of the database,the maximum deviation between reproduced and original models exceeds 5% (at somewavelengths, but without inspecting at which one). Considering each database modelwas calculated accurately to within 5%, we conclude that although ambitious, theANN approach can produce signicant dierences between database and replicated

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models. Figure 4.4 shows a Clumpy model SED in two versions. The black line isthe model in its original form, as computed by Clumpy, while the red one is theANN-reproduced version for the same set of parameter values. This is the singlemodel with the worst match between DB and ANN-models, and all other originalmodels are reproduced more faithfully. However, this uncontrolled introduction ofnew uncertainties must be dealt with before the elegant ANN approach can be usedwithout concerns.

Optimizing both the complexity and the training phase of the underlying ANNcould lead to a better agreement, but we have not undertaken this in the currentwork. We instead proceed with an approach to interpolate the SEDs directly and in6 dimensions.

4.4.5.2 Direct multi-dimensional interpolation

Advances both in hardware speed and in the availability of software libraries makeit now possible to attempt a direct N-dimensional interpolation of our torus modelsat any location in the volume covered by the parameters in the DB. Using functionsfrom the Scipy4 package for Python I have implemented a fast and generic N-diminterpolator. Many functions in Scipy that work with unstructured/scattered dataare much too slow (because they have to grid the data rst). The ones that arefast, on the other hand, expect regularly gridded data. The Clumpy parameters aresampled on a rectilinear grid, but it is not regular (the dierence is that in regulargridding all parallelepipeds making up the grid are congruent, whereas in a rectilinearbut not regular grid they are not). We thus perform a transformation from the non-regular Clumpy coordinates into regular ones in the oating-point space of pixelcoordinates. On such a grid scipy.ndimage.map_coordinates() can then be usedfor fast interpolation of our 7-dimensional model SEDs (6 free Clumpy parametersplus the wavelength axis).

It is important to point out that when the data (or the models in our case) coverorders of magnitude in dynamical range, any interpolation should be rather performedin logarithmic space. As Figure 4.5 shows for a simple case (a power-law y(x) = 1/x3),interpolation in the linear domain can lead to unexpected behavior. The blue dots inthe gure follow the power-law and are spaced one per decade. An attempt (shownin red) to insert 10 new points between each adjacent pair of blue dots via linearinterpolation in the linear-linear domain (both x and y are used as-is) leads to verynon-linear results when plotted on the log-log scale again. More successful is the2nd attempt (shown in green), where the original data has been logarithmized rstbefore a linear interpolation was performed. Afterwards, the resultant intermediatevalues have been de-logarithmized again. As the gure shows, this yields the expectedbehavior.

Our N-dimensional direct interpolation scheme is very fast. On a modern CPU(Intel Core2Duo i5), and if all 6 Clumpy parameters are taken to have uniform

4http://www.scipy.org/

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100 101 102 103 104

x

10-12

10-11

10-10

10-9

10-8

10-7

10-6

10-5

10-4

10-3

10-2

10-1

100

y

y = x−3

datalinear interpolationloglog interpolation

Figure 4.5: Linear interpolation of intrinsically logarithmic data y(x) = 1/x3 (bluedots). When the data are linearly interpolated in linear-linear space, the resultantintermediate values (red crosses) show a distinctly non-linear behavior in double-logarithmic space. Logarithmizing the data, then performing the linear interpolation,and nally de-logarithmizing the results gives the expected outcome (green crosses).

priors, ∼2000 samples/s can be drawn. With 105 MCMC samples being a comfortablenumber of samples for obtaining smooth posteriors, a single SED can be modeled inwell under a minute.

4.4.6 Application & Results

I have written an MCMC code based on PyMC for performing Bayesian inference ofparameters for AGN SEDs tted with the Clumpy torus models. If desired, anaddition of a blackbody component is user-selectable, as is also the inclusion of dustextinction in the modeling. Both additions, if selected, each introduce one new freeparameter to the model. The user can select for each parameter what kind of prioris to be used while sampling (currently a uniform prior, a truncated Gaussian, and aDelta function are implemented). The code is optimized such that all priors of sametype (e.g. 'uniform') are vectorized, and updated by the sampler simultaneously. Thisincreases the sampling speed tremendously. We nd that the speed penalty growslinearly with the number of dierent types of priors being used, but almost not at allwith the number of parameters. In the ideal case when all sampled parameter priorsare of identical type, ∼2000 samples/s can be easily achieved on modern hardware.This is certainly fast enough for practical applications, despite the fact that a full N-

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10-2 10-1 100 101 102 103wavelength [µm]

10-16

10-15

10-14

10-13

λFλ[W

/m

2]

zoom

i = 90.00τv = 23.35q = 0.50N0 = 15.00σ = 70.00Y = 26.83χ2 = 8.7302χ 2r = 0.3358

MAP modeldata

101wavelength [µm]

10-14

10-130 100000 200000 300000 400000 500000

First iteration

3

2

1

0

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Gew

eke

z-sc

ore

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. dev

iatio

ns)

itvq

N0sigY

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sam

ple

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ber

0 15 30 45 60 75i

0.00

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prio

r & p

oste

rior

best fit = 90.00median = 77.95mode = 88.501σ = [63.0,87.0]2σ = [51.0,90.0]DKL = 0.95

posteriorpriorbest fit

median1σ interval2σ interval

50 100 150 200 250τv

0.00

0.01

0.03

0.04

0.05best fit = 23.35median = 33.46

mode = 34.171σ = [19.7,48.7]2σ = [19.7,48.7]

DKL = 2.27

0.5 1.0 1.5 2.0 2.5q

0.00

0.26

0.52

0.79

1.05best fit = 0.50median = 0.94

mode = 1.051σ = [0.4,1.4]2σ = [0.0,1.6]

DKL = 0.69

2.5 5.0 7.5 10.0 12.5N0

0.00

0.19

0.38

0.57

0.77best fit = 15.00median = 14.21mode = 14.771σ = [13.1,15.0]2σ = [11.7,15.0]DKL = 1.66

20 30 40 50 60σ

0.00

0.05

0.09

0.14

0.18best fit = 70.00median = 66.64mode = 69.081σ = [60.8,70.0]2σ = [57.2,70.0]DKL = 1.63

20 40 60 80 100Y

0.00

0.02

0.03

0.05

0.07best fit = 26.83median = 34.73

mode = 28.751σ = [27.2,58.8]2σ = [24.0,93.7]

DKL = 0.76

centralnewerror18_clumpygrid_20120122.txt

Figure 4.6: Example of tting the Subaru SED of Cygnus A with our MCMC-sampling/tting code (data courtesy of Merlo et al., 2012, in prep.). The top leftand top middle panels show the tted data (with error bars) and the MAP (best-t)model. The lower half of the gure shows, in 6 sets of 2 panels each, the traces (upper,106 samples) and marginalized posteriors (lower) for all 6 modeled Clumpy parame-ters. Results of the statistical analysis are printed in the legends of the lower panels.Note how the Kullback-Leibler divergence DKL determines how well each parameterwas constrained. The red line in the lower panels shows the priors that were used perparameter.

dimensional interpolation of model SEDs is performed at each step (Section 4.4.5.2).As an illustrative example Figure 4.6 shows the results of running the code to

model the Subaru Mid-IR SED of Cygnus A, a prominent type-2 AGN (data courtesyof Merlo et al., 2012, in prep.). The top left panel (the top middle panel is just azoomed version) shows the data (in gray color, with error bars), and as a black linethe MAP (best-t) model. The six sets of 2 panels in the lower half of the gureshow the traces and marginalized posteriors for the six Clumpy parameters. Thetraces are nicely converged, and the posteriors seem to behave smoothly. All relevantstatistical data are printed in the lower panel legends.

The important question to answer is how well each parameter could be constrainedfor the SED being modeled. It is easy to see that the shape of the posterior histogramsmust hold the key to answering this question. If we remember that the selectedpriors for all parameters were at (shown as a red line in the lower panels), yet afterintroducing the data they all dier from a at distribution, it becomes clear that the

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reason for this deviation comes from the likelihood term in Eq. (4.8).A measure for the deviation of a prior from its posterior is the Kullback-Leibler

divergence (Kullback and Leibler, 1951)

DKL =

∫t(x) ln

t(x)

p(x)dx, (4.13)

with the prior p and posterior t both probability density distributions (PDF) of a ran-dom variate. See Appendix C for a deeper discussion on the properties the Kullback-Leibler divergence. The lower limit of DKL is 0, and occurs only when p and t areidentical. When understood as an information gain (see, e.g.: MacKay, 2003, andalso Appendix C), DKL = 0 signals that the introduction of data did not constrain aparameter at all. On the other extreme, the more a posterior deviates from the prior,the larger DKL will grow.

The Kullback-Leibler divergence is a parameter-independent quantity, and I showin Section C.5 that it is invariant under parameter transformations. It can thereforebe used as-is to compare the deviations of priors and posteriors among all modeledparameters. Given the uniform priors on all Clumpy parameters, the larger the DKL

value, the more a posterior deviates from the prior, and the better this parameterwas constrained by tting the data. For the example shown in Figure 4.6 the best-constrained parameter was τV (with DKL = 2.27), followed by N0 and σ (both almostequivalently constrained), followed by i, Y , and nally q.

4.4.7 MCMC chain convergence

In theory a Markov chain must eventually converge to an equilibrium posterior densitydistribution, but depending on model complexity and sampling eciency this canrequire a long time. Especially if the N-dimensional posterior has multiple distinctmodes, the time between jumps of the chain from one mode to another can be verylong. While some authors, surely only semi-seriously, suggest to run a single chain formonths at a time, the best way to increase the chances for convergence in reasonabletime is to run multiple MCMC chains with dierent starting locations in the N-dimensional parameter space, and to monitor the intra-chain and inter-chain variancein these chains. Brooks, Gelman, and Rubin introduced a convenient diagnostic, andwe employ in the following a notation similar to Gelman et al. (2004). For each scalarestimand θ (recall that the full parameter vector was θ = (θ1, . . . , θNpar)) we candenote a given draw from J parallel chains of length n as θij(i = 1, . . . , n; j = 1, . . . , J).We can then measure the between- and within-sequence variances B and W of thechains as

B =n

J − 1

J∑j=1

(θ.j − θ..)2, where θ.j =1

n

n∑i=1

θij, and θ.. =1

J

J∑j=1

θ.j (4.14)

W =1

J

J∑j=1

s2j , where s2

j =1

n− 1

n∑i=1

(θij − θ.j)2. (4.15)

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The θ.j in Eq. (4.14) are within-sequence means. The marginal posterior variance ofeach scalar estimand θ can then be calculated as a weighted average of B and W

var(θ|y) =n− 1

nW +

1

nB. (4.16)

It overestimates the true variance when assuming that the J starting positions areoverdispersed5, but it is unbiased if the MCMC chains have converged to an equi-librium distribution (or when n → ∞). With W and B we can now compute thepotential scale reduction factor

√R =

√var(θ|y)

W. (4.17)

It declines to unity as n→∞. When its value is not close to 1 the chains should beallowed to run longer. Alternatively, or in addition, the MCMC jumping rule mightneed to be adjusted to allow for more ecient sampling. This monitoring shouldbe performed on each scalar model parameter separately, ensuring that all of themdecline to 1 as n grows larger. We have implemented a rst version of the Brooks-Gelman-Rubin diagnostic, and will report its behavior in our applications elsewheresoon.

4.4.8 Y(q) sampling

In their simplest form, the six Clumpy parameters are all physically independentof each other, and when sampling them with MCMC algorithms one can focus onevery parameter separately. The physical reality however demands some adjustmentto this assumption. Recall from Section 4.1 the denition of the parameters Y andq. Y is the ratio of torus outer and inner radii, while q describes how the cloudsare distributed along any ray in radial direction according to a power-law 1/rq. Itbecomes evident that when q is 0 (or close to that value) then there will be equallymany clouds per unit length along a radial ray both close to and far away from thecentral AGN. When q is large (say e.g. q = 3), the power-law is very steep, and thevast majority of all clouds will be concentrated very close to the inner torus radius.

From the fact that along a radial ray N clouds are distributed between the tworadii r = 1 and r = Y , the radius rf can be derived within which a fraction f of allN clouds is contained

rf =

10f · log10(Y ) if q = 1(

1− f · Yq−1 − 1

Y q−1

) 1

1− q if q 6= 1.

(4.18)

5Overdispersion means that the starting positions are chosen such that their variance is largerthan what would be expected if they were distributed purely according to the posterior distribution.

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0.0 1.0 2.00

1

2

3

4

5

Y=

5

fN0=0.500

0.0 1.0 2.0

fN0=0.700

0.0 1.0 2.0

fN0=0.900

0.0 1.0 2.0

fN0=0.950

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fN0=0.990

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fN0=0.999

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2

4

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Y=

10

0.0 1.0 2.0 0.0 1.0 2.0 0.0 1.0 2.0 0.0 1.0 2.0 0.0 1.0 2.0 3.0

0.0 1.0 2.005

1015202530

Y=

30

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10

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Y=

50

0.0 1.0 2.0 0.0 1.0 2.0 0.0 1.0 2.0 0.0 1.0 2.0 0.0 1.0 2.0 3.0

0.0 1.0 2.0q

0

20

40

60

80

100

Y=

100

0.0 1.0 2.0q

0.0 1.0 2.0q

0.0 1.0 2.0q

0.0 1.0 2.0q

0.0 1.0 2.0 3.0q

Figure 4.7: Radius rf (q;Y, f) within which a fraction f of all clouds on a radial rayis contained. The radius depends on the Clumpy parameters Y and q, and on thedesired fraction f . rf is shown in red. The columns are for dierent fractions f ,and the rows for dierent values of Y . The gray-shaded areas must be excluded fromsampling: all regions above the red line are excluded by Eq. (4.18), and all regionsbelow the dashed horizontal line at rf = 5 are excluded by the fact that the Clumpydatabase only contains models with Y ≥ 5.

This radius depends on Y , q, and f , but note that it is independent of the number ofclouds; only the ratio of clouds contained within rf and the total number of cloudsmatters, and therefore cancels out.

Figure 4.7 shows rf as a function of q (as a red line). The columns of the gureare for the dierent fractions f = 0.5, 0.7, 0.9, 0.95, 0.99, 0.999. The rows are eachfor dierent values of the Y parameter (Y = 5, 10, 30, 50, 100). For instance in thelower left panel the red line shows that for a torus with Y=100 and q=0, 50% of allclouds (f = 0.5) are located at radii ≤ 50. The same line also shows that at q ∼ 1.25

that same fraction of 50% of all clouds is contained within a radius of . 5. If oneasked for a fraction of 95% of all clouds, for a torus with Y=100 and at q=2, thecontaining radius is ∼ 18.

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Figure 4.8: Sampling from Y (q). A total of 105 samples were drawn, assuming uniformpriors on q and Y . A scatter plot of the Y versus q sampled values is shown. Thesampling was performed uniformly and over the entire ranges of both parameters, butthe log-likelihood was set to −∞ each time when Y left the range permitted by Eq.(4.18). The result is a uniform sampling over the 2d-space spanned by q and Y (q).The exclusion zones eectively form innite "walls" which the sampler cannot cross.f = 0.99 and Y = 100 were used for this gure.

It is clear that sampling both Y and q independently could lead to a bias, andto erroneous inferences. One must account for this Y (q) dependence in the priors.Therefore, the sampling code must somehow be made aware of the dependence of Yon q. Care must be taken of the fact that the sampling follows the user-selected priorfor each parameter, even though they might be internally linked. Figure 4.8 showsthe result of exploiting the Y (q) dependence in the priors during sampling in a toyexample (no data, just sampling from the priors).

The sampling was performed uniformly on both parameters (as the priors on bothq and Y were chosen uniform), and from their full ranges. The returned log-likelihood,however, was modied to −∞ whenever the randomly sampled value for Y was > rf .The log-likelihood was also set to −∞ when the sampled Y value was below 5, sincethis is the smallest available value for Y in the Clumpy database. Both areas ofexclusion dictated by Eq. (4.18) and by the Y ≥ 5 values present in the DB areshaded gray in Figure 4.7. The sampling must occur from the areas left white in thegure. As the gure shows, this sampling explores the Y (q) space uniformly in 2d.

4.4.9 Parameter correlations

The marginalization of the multi-dimensional likelihood function (Eq. (4.10)) over allbut one of the sought-after quantities is only one possibility of the Bayesian approach,although certainly the most common. One can, however, marginalize over all but two

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20

30

40

50

60

sig

2.5

5.0

7.5

10.0

12.5

N0

0.5

1.0

1.5

2.0

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q

25

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tv

15 30 45 60 75 90Y

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30

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60

75

i

20 30 40 50 60sig

2.5 5.0 7.5 10.0 12.5N0

0.5 1.0 1.5 2.0 2.5q

25 50 75 100 125tv

Figure 4.9: 2d-marginalized posteriors for all unique pairs of Clumpy parameters,after tting the Subaru Mid-IR SED of Cygnus A (data courtesy of Merlo et al., 2012,in prep.). Uniform priors were assumed on all parameters. The color scale encodesthe two-dimensional probability density function, and ranges from dark blue (=0) tored (at peak value).

such parameters, ending up with a two-dimensional posterior probability distribution.

For all unique pairs of Clumpy parameters such two-dimensional cuts throughthe full six-dimensional likelihood function are shown in Figure 4.9. The tted SEDwas that of Cygnus A introduced in Section 4.4.6. The color scale (dark blue to red)encodes the probability density, normalized to its peak value. Such two-dimensionaldistributions are very useful in recognizing correlations between tted parameters.For example, from the τV , q panel it is clear that the two parameters are highlycorrelated upon exposure to the given data. In the q, Y panel most of the mass ofthe posterior seems concentrated along a narrow band in the 2d-space.

Note that the appearance of this gure will change every time a dierent datasetis modeled, because the shown posteriors are the product of both the priors (modelDB, always the same) and observed data. In Section 4.5 we will investigate how wellthe parameters can be constrained, knowing that there are inherent degeneracies inthe model parameter space, even without introduction of data to the problem.

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4.4.10 Theory selection

We have seen in Section 4.3.1 that sometimes it may become necessary to t anobserved SED with more than just one synthetic SED component. In the case ofthe quasar SEDs from Deo et al. (2011) (see Figure 4.1) composites of torus andblackbody SEDs provided ts that were much superior to torus-only models. In theformer case the model had 7 free parameters, in the latter 6.

However, the addition of more degrees of freedom to the problem need not al-ways be the right approach. To exemplify this, we tted the Spitzer SED of blazarPG1222+216 (Malmrose et al., 2011b) with several models of varying complexity.By inspection, the SED resembles a blackbody-like shape once a power-law was sub-tracted from it to remove the jet's contribution and reveal the torus signature. Inaddition to the torus+BB composite modeling (1) and a torus-only tting (2), wehave tted this SED with three other approaches: (3) a single-temperature BB-onlymodel (unmodied Planck function), (4) a κλBλ(T ) optically thin BB emission model,and (5) an optimal combination of (3) and (4). κλ is the dust opacity curve, moreaccurately the absorption part of it. The neglected scattering part of the opacitycurve would only aect wavelengths . 2µm.

Panels (1), (3a) and (4a) of Fig. 4.10 show the same data of PG1222+216 as blackdots with error bars. Each of these panels also plots the best-t model resulting fromany of the ve discussed tting approaches. In panel (1) the three solid lines representthe best-t obtained with any of the single-component methods: blue is the torus-only model, red stands for the single unmodied BB t, and green is the opticallythin BB emission (modied Planck function). Remarkably the two torus-free SEDsare better ts than the torus model, especially the unmodied single-temperature BBwith its χ2

r = 2.37. The hot temperature (TBB = 1301 K) of this BB allows its SEDto peak exactly where the NIR-dominated spectrum has its maximum, but due toits unmodied nature the BB function fails to reproduce the silicate features around10µm and 18µm. Both the torus-only and the modied BB models also resemble theNIR suciently well, but show too strong 10µm silicate feature strengths.

The black line in panel (3a) of Figure 4.10 shows the optimal linear combination(obtained by minimizing Eq. (4.5)) of a torus component (blue) and a single unmodi-ed BB spectrum (red). The overall t quality is much improved by this combination,and χ2

r is down to 1.24 from 17.05 for the best torus-only model, and still almost afactor of 2 better than the single BB t. In this composite model the BB again pro-vided the bulk of ux in the NIR, while the torus component enabled a much nerreproduction of the silicate features in the overall model. The BB fraction in the IRis fBB = 0.73. Panel (3b) graphs the fractional contributions Bi/Mi and Ti/Mi of thetwo components to the total model M as a function of wavelength, their sum beingunity by denition. The 1394 K hot BB dominates in the NIR region, while the torusis of comparable relative importance in the MIR.

The single BB model in panel (1) outperformed both the torus as well as themodied BB models, and in a torus+BB t the BB is the signicantly more domi-

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0.1 1 10 100λ [µm]

10-17

10-16

10-15

10-14

λFλ

[Wm−

2]

(1)

re-binned datatorus, χ 2

r =17.05BB (1301 K), χ 2

r =2.37opt. thin BB (897 K), χ 2

r =5.10

0.1 1 10 100λ [µm]

10-17

10-16

10-15

10-14

λFλ

[Wm−

2]

(3a)

BB (1394 K)torusBB + torus, χ 2

r =1.24

0.1 1 10 100λ [µm]

10-17

10-16

10-15

10-14

λFλ

[Wm−

2]

(4a)

BB (1483 K)opt. thin BB (640 K)BB + opt. thin BB, χ 2

r =0.87

0.1 1 10 100λ [µm]

0.6

0.7

0.8

0.9

1.0

1.1

1.2

1.3

1.4

(BB

+ to

rus)

/ (B

B +

opt

. thi

n BB

) (2)

(3a) / (4a)

0.1 1 10 100λ [µm]

0.0

0.2

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1.0

frac

tiona

l con

trib

utio

n

(3b)

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0.1 1 10 100λ [µm]

0.0

0.2

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0.6

0.8

1.0

frac

tiona

l con

trib

utio

n

(4b)

BB from (4a)opt. thin BB from (4a)

Figure 4.10: Fits to Spitzer data of PG1222+216. Panels (1), (3a) and (4a) all showthe same re-binned data as black dots with error bars. Each panel also depicts the bestts obtained with dierent models. The χ2

r values are given in the legends. (1) Best-t model using either a single Clumpy torus model (blue), or a single unmodiedblackbody (BB) spectrum, with temperature T = 1301 K (red), or a single opticallythin BB emission spectrum κλBλ(T ), with T = 897 K (green). (3a) Best compositemodel (black) of a torus (blue) and an unmodied BB component (red). The BBtemperature is 1394 K. (3b) Fractional contribution of the two components frompanel (3a) as a function of wavelength λ. Their sum is by denition unity. (4a) Bestcomposite model (black) of an unmodied BB component (red), and a secondary,optically thin BB emission (green). The temperatures of the two BBs are 1483 K and640 K, respectively. (4b) As panel (3b), but for the two components from (4a). (2)Ratio of the two composite models (each black curve) from panels (3a) and (4a). Itis very close to unity for λ & 2µm.

nant component. Because of these observations we have attempted two-componenttting that comprises an unmodied BB, with the addition of some optically thinBB emission which could help the composite model to perform well in the MIR. Theresulting best-t of this procedure is shown in black in panel (4a) of Figure 4.10. Theχ2r value improves further, now being 0.87. The two blackbody constituents of the

model are drawn in red (unmodied BB, TBB = 1483 K) and green (optically thin BBemission, TBB = 640 K.). Panel (4b) shows the fractional contributions of these twocomponents. Apart from the shortest wavelengths this panel very much resemblespanel (3b). Indeed, the similarity of both the composite ts shown in panels (3a)and (4a) is striking. We show their ratio versus wavelength in panel (2) of the gure.

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Beyond & 2µm this curve is close to unity.Looking only at these best-ts for the moment it is evident that the simple two-

component model (BB + optically thin BB), with its two free parameters (the BBtemperatures) outperforms the other two-component theory (torus + BB), one whichhas 7 free parameters available to satisfy the data. Clearly, in the case of PG1222+216a torus does not represent the best possibility. A simple combination of hot dust (≈1480 K) and some cooler optically thin dust emission (at 640 K) is better suited toexplain the data.

Inspecting only the best-t models in each case does of course not tell the wholestory. It must be noted that the theoretical model chosen to t a set of data oughtto be reasonably close in its predictions. If SEDs generated by a set of parametersare very dierent from the data they were supposed to t, then their χ2 values arevery large. Therefore the likelihood in Eq. (4.10) becomes very small, even easilycomputationally zero. If this is the case for a large fraction of the parameter space,much interpretative power is lost.

Being faced with such a situation might hint at the possibility that the proposedtheoretical model is not quite good enough to explain the observed data. A dier-ent theory, probably one that introduces additional parameters, could explain theobservations better. A second important application of Bayesian analysis emergeshere, the so-called Bayesian selection of competing theories. Bayesian theory selec-tion provides a mathematical approach in assessing what theory to prefer in light ofthe data, given two or more theories of dierent complexity. Obeying Occam's razor

one ideally wishes to chose the simplest of all proposed theories that explains thedata suciently well. Both the too simple and the too complex models should bepenalized, and the preferable theory is the one that nds the best balance betweenaccuracy of its predictions and complexity.

Although it can be dicult to calculate the Bayesian evidence Px(D) of a theoreti-cal model X, given the data D, the most consistent way of comparing the performanceof two competing theoretical models A and B is to calculate the ratio of their evidences(see, e.g., Trotta, 2008), often called the Bayes factor

RAB =PA(D)

PB(D). (4.19)

The data D are of course the same in both cases. A commonly used empirical logarith-mic scale for Bayes factors is "Jereys' scale" (Jereys, 1998). It helps in evaluatingthe preference that one should give to one theory over another. An implementationof the scale is given in Trotta (2008, Table 1 therein). It names the strength ofevidence for a theory A over another theory B 'inconclusive' if lnRAB < 1, 'weak'when lnRAB = 1, 'moderate' if lnRAB = 2.5, and 'strong' when lnRAB = 5. Weare currently in the process of computing the evidences for tting the Deo et al. andMalmrose et al. data, but this requires to use other sampling techniques, like nestedsampling. We will report the results elsewhere.

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However, alone from the (in some cases very poor) best ts obtained with thedierent combinations of torus and blackbodies, it can be safely argued, that thejet-subtracted SED of PG1222+216 is not very well described by only a dusty torus.A much simpler one-parameter (BB only) or two-parameter (BB+optically thin BB)model provides a better t overall. In comparison with approach (5), the torus+BBtting (1) is competitive enough to be considered, but in light of its 7 free parametersit should be discarded in favor of the simpler theory (5) with just two free parameters.It should also be pointed out that none of the two single-BB models (unmodied ormodied Planck function) performs nearly as well as the optimal combination of twosuch blackbodies.

4.5 Degeneracies

The radiative transfer problem for heated dust is inherently degenerate (Vinkovi¢et al., 2003). Constraining the parameters is not possible from the spectral energydistribution (SED) alone. A toroidal and clumpy geometry introduces further ambi-guities due to the relatively large number of required parameters, thus the space ofmodel parameters suers from degeneracies. Even without introducing any data tobe t by the models there is a level of uncertainty, if one were to sample randomlyfrom the parameter space, and attempted to deduce from the synthetic SED whatparameter values generated this SED. One must distinguish formally between twolevels of uncertainty: uncertainty in parameter estimation this is due to uncertaintyin the data, and parameter unidentiability which is caused by true degeneraciesin the parameter space. The latter of these two eects leads to the curious fact thateven with "perfect" data (with innitely small error bars) the particular set of modelparameters which generated a best-t to the data might not be unique.

We have devised a way of quantifying the degree of degeneracy that is presentin the Clumpy model DB, by temporarily treating the models themselves as if theywere data SEDs to be t. The procedure is outlined as follows

1. Draw a random set of Clumpy parameter values.

2. Retrieve the model SED corresponding to these parameters, interpolating ifnecessary (Section 4.4.5.2).

3. Introduce random Gaussian noise of given amplitude to the model uxes (errorbars). Do this for ever-smaller error amplitude.

4. Perform full MCMC sampling and Bayesian inference on this noisy model, as ifit were data.

5. Store characteristics of the recovered results (e.g. mean & mode & credibleintervals of the marginalized posteriors, etc.)

6. Repeat for many random models.

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10-1 100 101 102

λ[µm]

10-3

10-2

10-1

100

λFλ

[arb

itra

ryunits]

10-1 100 101 102

λ [µm]

0.01

10-1 100 101 102

λ [µm]

0.05

10-1 100 101 102

λ [µm]

0.10

10-1 100 101 102

λ [µm]

0.20

10-1 100 101 102

λ [µm]

0.30

10-1 100 101 102

λ [µm]

0.50

Figure 4.11: Clumpy SED for a randomly drawn set of model parameter values. Inthe left panel the original SED without noise is shown in gray. In the other panelsthe individual ux levels are perturbed by adding Gaussian-random noise of givenamplitude. The error levels are printed atop the panels. The error bars are shown inblue.

7. Measure how well the original parameter values were recovered in the analysisfor a large sample of random models.

Step 1 is trivial, and step 2 can be easily accomplished with the techniques devisedin Section 4.4.5.2. For step 3, the introduction of error bars to the model uxes,we must rst understand what denes the amplitude of noise in a signal. Usually,observational data result from measuring some physical signal with an inherently noisydevice. For SED uxes, this is most often a CCD, which suers from several sourcesof noise, e.g. read-out noise, thermal noise, uneven CCD illumination, CCD eciencyvariations, and others. In typical astronomical applications, the combined eects ofthe dierent sources of noise prevent the level of measured ux to be determinedexactly. The strength of noise from all noise sources is then estimated and the dataare released with so-called 1σ-errors, stating also that the ux is accurate to within,say, 10% of the ux value.

We use this denition in our procedure to generate randomized error bars forthe uxes of the Clumpy models. For any ux value fi at some i-th wavelength, arandom number from a Gaussian, centered on 0 and of width σi = errorlevel · fi, isdrawn. We make sure, and have veried, that the Gaussian is normalized such that ifthe random number is drawn a very large number of times from the same Gaussian,it falls 68.3% of the time into the 1σ-range around the mean. This randomly drawnnumber is then added to fi, thus perturbing the clean model ux up or down. Thelength of the error bars at this ux is of course errorlevel · fi, but the ux level is nowrandomized. For a random model obtained in steps 1 and 2, we generate six noisyversions at these error levels: 0.01, 0.05, 0.1, 0.2, 0.3, and 0.5. Figure 4.11 shows inall panels one (and the same) randomly drawn Clumpy model SED. In the left-mostpanel the model is plotted as a gray line without any noise. This is the version asit was interpolated from the Clumpy DB. The subsequent panels add randomizednoise, whose amplitude is a fraction of the ux values (calculated separately per

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wavelength). The error levels of this Gaussian are printed atop every panel. Theerror bars are shown in blue color.

We then move on to steps 4 and 5, and perform a full MCMC sampling andBayesian parameter inference on each of the noisy versions of the model, afterwardsstoring the main results (e.g. the characteristics of the posterior, etc.). We repeatthis procedure for a large number of models, in this case 105. The fact that 105

random models had to undergo a full Bayesian inference procedure, each in the 6noisy versions outlined above, and that we decided to draw 105 samples each time

(plus 104 samples for the burn-in phase) to obtain suciently smooth posteriors,eectively required 6.6 · 1010 random samples to be drawn by the MCMC sampler.At a speed of ∼2000 samples/s quoted in Section 4.4.5.2 for modern hardware, thisis no trivial undertaking. We parallelized the entire procedure on the level of singlemodels, and ran the code on the DLX supercomputer at the University of Kentucky.The resulting output les were available after ∼ 2 days of calculations. It should benoted that we would ideally like to perturb each individual model, at each individualerror level, more than one time. However, another factor of 104 or 105 is too much,even for a supercomputer.

The major result of this computation is summarized in Figure 4.12. The gurehas 6 columns of panels, one column per sampled Clumpy parameter. At each row ofpanels, from top to bottom, an increasing error level of the noise that was added to themodels is shown. Every individual panel shows as a 2d-histogram the distributionof the originally sampled parameter value (on the x-axis) vs. the median value ofthe marginalized posterior for that parameter (y-axis), for all 105 randomly drawnmodels. The color scale (increasing from white to dark red color) encodes the densityof the results. Contour lines (in light gray) are overplotted, at levels of 3,10,30,50,70,and 90% of the peak density.

If a parameter were perfectly recovered each time, the 2d-histogram should beexpected to show a very narrow straight line from the bottom left to the upper rightcorner of the panel. Given the degeneracies and the error bars introduced to themodels this is of course never the case. At small error levels we see, however, resultsthat are very close to the ideal case. At 1% error level the majority of models fall in anarrow band around the 1:1 line for all parameters. There are already some dierencesin the distribution of the histograms visible between the Clumpy parameters, butonly at a small level.

Each panel is accompanied to its right by a 1d-histogram of the distribution alongthe y-axis. The histograms along their x-axes are always at, because they are thetrue sampled parameter values, and these were sampled uniformly. We thereforedo not plot the x-axis histograms. From the y-axis histograms, however, a goodassessment can be made in each case about the shape of the distribution of therecovered median values. The more a histogram deviates from a at distribution, theworse the recovered parameters values, on average, resembled the true values.

We see both from the 2d density maps and from the 1d-histograms how the quality

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100

200

300

[med

ian]

erro

rs 1

%

1

2

3

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edia

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erro

rs 5

%

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0%

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rs 3

0%

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10 100 200 300τavg [sampled]

10

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[med

ian]

erro

rs 5

0%

0 1 2 3q [sampled]

0

1

2

3

1 5 10 15N0 [sampled]

1

5

10

15

10 40 70 100Y [sampled]

10

40

70

100

0 30 60 90i [sampled]

0

30

60

90

15 30 50 70σ [sampled]

15

30

50

70

Figure 4.12: 2d-histograms of recovered medians of the marginalized posteriors (ony-axis) vs. the true sampled model parameter values (on x-axis), for 105 randomly se-lected Clumpy models. Each column shows the 2d-histograms for one of the Clumpyparameters, with increasing error level from top to bottom. The color scale, rangingfrom white to dark red, encodes the model density in the 2d-histogram and is normal-ized to the peak value. Density contours are overplotted in light gray at 3,10,30,50,70,and 90% of the peak. 1d-histograms to the right of each panel show the distributionalong the y-axis. Horizontal 1d-histograms (along the x-axis) are not shown, becausethey are at in all cases due to the uniform sampling of model parameters.

of parameter recovery decreases for each parameter with growing error level. The bandaround the 1:1 line broadens, and in some cases even breaks up into disjoint islands.The accompanying histograms conrm this more clearly: the marginalized posteriorsdeviate more and more from a uniform shape, and even become bimodal for someparameters (most strongly in σ).

Although both the uncertainty due to errorbars and due to parameter unidenti-ability contribute to the widening of the diagnostic histograms, it is clear that someparameters suer more from ever-increasing error amplitude than others. Even at thesmallest error amplitudes the recovery is not of identical quality for all parameters.This is an expression of the unidentiability eect.

The most striking impression is that some of the parameters, in particular τavg

and q, seem to retain a good level of coherency even at large error levels. Apparentlythese parameters suer least from intrinsic degeneracies. To quantify the impressionswe plot in Figure 4.13, in a conguration identical to Figure 4.12, histograms ofδX = Xmedian − Xsampled values of any parameter X, i.e. a correlated distributionof the deviations of recovered values from the true model values. To compare thehistograms between dierent parameters more easily, we scale δX by the range of the

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0.5

1

model

s/bin

FWHM = 0.030

erro

rs 1

%

FWHM = 0.042 FWHM = 0.049 FWHM = 0.049 FWHM = 0.053 FWHM = 0.055

0.5

1m

odel

s/bin

FWHM = 0.049

erro

rs 5

%

FWHM = 0.054 FWHM = 0.073 FWHM = 0.070 FWHM = 0.101 FWHM = 0.138

0.5

1

model

s/bin

FWHM = 0.061

erro

rs 1

0%

FWHM = 0.087 FWHM = 0.105 FWHM = 0.097 FWHM = 0.148 FWHM = 0.207

0.5

1

model

s/bin

FWHM = 0.081

erro

rs 2

0%

FWHM = 0.129 FWHM = 0.139 FWHM = 0.161 FWHM = 0.214 FWHM = 0.300

0.5

1

mod

els/

bin

FWHM = 0.091

erro

rs 3

0%

FWHM = 0.164 FWHM = 0.178 FWHM = 0.258 FWHM = 0.263 FWHM = 0.331

-0.4 -0.2 0 0.2 0.4δτavg/∆τavg

0

0.5

1

mod

els/

bin

FWHM = 0.124

erro

rs 5

0%

-0.4 -0.2 0 0.2 0.4δq/∆q

FWHM = 0.214

-0.4 -0.2 0 0.2 0.4δN0 /∆N0

FWHM = 0.239

-0.4 -0.2 0 0.2 0.4δY/∆Y

FWHM = 0.456

-0.4 -0.2 0 0.2 0.4δi/∆i

FWHM = 0.339

-0.4 -0.2 0 0.2 0.4δσ/∆σ

FWHM = 0.399

Figure 4.13: Histograms of δX = Xmedian−Xsampled for any Clumpy parameter X, innatural units ∆X = Xmax−Xmin allowing for direct comparison between parameters.All histograms are normalized to unit area. The peakiness and width of a histogramis a measure of the level of degeneracy present for this parameter in the database(and at the given error level). The full-width-at-half-maximum (FWHM) is printedin every panel.

parameter ∆X = Xmax−Xmin, thus expressing them in natural units. The histogramsare normalized to unit area, and all are plotted such that the highest peak of all islabeled at 1.0. The peakiness of a histogram, or equivalently its width, describesquantitatively the level of degeneracy aicting the given parameter.

We measure the full-width-at-half-maximum (FWHM) for each histogram, andprint the value in the top left corner of every panel. Figure 4.14 plots FWHM as afunction of error level for each parameter. It is immediately evident from this plotthat our previous impression was correct, namely that the parameters τavg and q arethe ones suering the least amount of degeneracy. They both start at the lowestvalues of FWHM, and retain the lead to the highest error levels. N0, the number ofclouds per radial equatorial ray, is on a similar level as q, but at small error levels isslightly outdone by Y . Y loses out quickly at 20% error level and above, ending upas the one with highest degree of degeneracy. i and σ are unsurprisingly the worstcontenders at virtually all error levels except at 50%. This is so because they bothare parameters measuring angles along the same physical dimension in the model. It

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0 10 20 30 40 50error level [%]

0

0.1

0.2

0.3

0.4

0.5

FWH

M [n

atur

al u

nits

]

τavg

q

N0

Y

i

σ

Figure 4.14: Full-width-at-half-maximum (FWHM) of the histograms in Figure 4.13as a function of noise level that was introduced to the Clumpy models. Each param-eter's curve measures the degree of degeneracy present in the DB at the given errorlevel.

is easily possible to have the same number of clouds along the line of sight either atsmall i and larger values of σ, or reversely at viewing angles closer to the equator,but for a torus with a small σ.

In conclusion, with this massive computational eort we were able, for the rsttime, to quantify the amount of degeneracy present in the Clumpy model parameterspace. We are now able to answer this long-outstanding question, and nd thatfor ever-increasing error levels the parameters that best retain their potential to beunanimously recovered are τavg, the optical depth of a dust cloud, and q, the steepnessof the radial cloud distribution law. N0 is a close contender, while Y , σ, and i performconsiderably worse. Up to error levels of about 20%, Y can be rather successfullyrecovered, but reaches unacceptable levels of degeneracy at higher levels of noise. Toretain a good level of condence, we recognize that a level of noise in the data betterthan ∼ 10% of the ux values is required. Noise levels higher than that might preventreliable constraints to be put on the inferred model parameters.

4.6 Acknowledgments

I am indebted to my co-authors on Merlo et al. (2012, in prep.), especially MattMerlo, Eric Perlman, and Chris Packham, for allowing me to use their Subaru data of

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Cygnus A in two gures prior to publication, and for very illuminating discussions. Iam also very grateful to Alan Marscher and Michael Malmrose for the permission touse their PG1222+216 data. Many thanks to Rajesh Deo for feedback and discussionsthat helped in improving our tting procedures, and for his data. Thanks also to TanioDíaz-Santos and Rivay Mor for helpful discussions.

Copyright c© Robert Nikutta 2012

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Chapter 5

Conclusions

Both theory and observations have long hinted at the fact that the dusty tori whichsurround Active Galactic Nuclei (AGN) must be made up of a distribution of discreteclouds rather than have their dust smoothly distributed throughout. Nenkova et al.(2002, 2008a,b) were the rst group to develop a fully self-consistent treatment ofdust radiative transfer in a clumpy medium. We formalized this approach in ourcode Clumpy, which can compute a synthetic spectral energy distribution (SED) ofa clumpy AGN torus for a wide range of parameter values. This allowed our group toapply the formalism in many versatile studies, many of which I had the great pleasureto be part of.

In Nikutta, Elitzur, and Lacy (2009) (the subject of Chapter 2) we have shown thatClumpy models are capable of explaining several seemingly puzzling observations ofAGN made with the Spitzer space observatory. Among those was the detection ofthe 10µm silicate emission feature in emission in type-2 AGN. Clumpy models alsoeasily explained why the emission peaks of the silicate feature were often observedat wavelengths longer than the ∼ 10.0µm at which the opacity curves of standardinterstellar dust species peak. Finally, Clumpy models never produce very deepsilicate absorption features, and also the strength of their emission features is rathershallow. Both facts are observed in nature, but have caused serious problems to mostsmooth-density torus models previously used.

In the forthcoming Nikutta, Nenkova, Ivezi¢, and Elitzur (2012) and Nikutta,Messias, Nenkova, Ivezi¢, and Elitzur (2013) (see Chapter 3) we have calculated thephotometric colors of all Clumpy models in the WISE (Wide-eld Infrared SurveyExplorer) and Spitzer/IRAC lter systems. We showed that Clumpy models fallvery closely into the regions of the color-color space occupied by QSO and otherAGN observed by both instruments, and in addition that they follow almost preciselythe empirical outline set for AGN in Stern et al. (2005). Dusty shells (non-clumpy) onthe other hand seem to explain well the colors of other types of astronomical sources,among them asymptotic giant branch (AGB) stars and several classes of young stellarobjects.

The growing availability of fast hardware and sophisticated algorithms for Bayesianstatistical analysis make it now possible to compute by means of fast, direct, multi-dimensional interpolation the output of Clumpy models (and others) for any ar-bitrary combination of model parameter values. This eectively provides us with acontinuous parameter space, and enables us to perform Markov chain Monte Carlosampling of the unknown N-dimensional posteriors, when the database of models isexposed to observational data. This "tting" of data with our models then revealsthe full and the marginalized posteriors, allowing us to constrain the likely ranges of

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matching parameter values with a quantiable level of uncertainty. This itself being amajor achievement, we also addressed the long outstanding question of degeneraciesintrinsic to the model parameter space. Such a breakup in parameter uniquenessarises from the degenerate IR radiate transfer problem itself, and is enhanced bythe complex geometry of a clumpy torus. Through a signicant computational eortwe were able for the rst time to measure the degree to which any of the Clumpyparameters can be constrained in principle, not just by virtue of tting the modelsto contaminated data. This directly translates into recommendations for noise levelsthat should be achieved during observations and data reduction. (See Chapter 4)

An interesting mathematical problem was solved along the way (see AppendixA). When the model SED comprises more then one component (e.g. the combinedSEDs of an AGN torus and a hot blackbody spectrum), we show that, given theobserved data and the known spectral shapes of the component SEDs, the optimal

magnitudes of the components can be calculated analytically. Previously, virtually allauthors performed numerical minimization of this problem, or opted to hold some ofthe degrees of freedom at xed values.

We also demonstrate in Chapter 4 that modeling observational data with multi-component SEDs can often provide much better ts. This is very evident in the SEDsof several type-1 AGN, where a spectral bump that peaks at ∼ 2−4µm is not well re-produced by the current Clumpy torus models. Adding a hot blackbody componentto the mix amends this aw in many cases, and we have identied the most likelysource for this shortcoming of our modeling. We warn, however, to blindly introduceever more free parameters, at the danger of overtting the data with unjustiablycomplex models.

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Appendix A

Analytical scales of SED components

We wish to t a set of data uxes di, observed at wavelengths i ∈ 1, . . . , Nλ, witha multi-component model SED. The total SED is constructed as a linear combinationof Nc separate components j ∈ 1, . . . , Nc

Mi =Nc∑j=1

Xjcji , (A.1)

with Xj the unknown scale of the individual components, and cji the ux of thej-th component at i-th wavelength. The spectral shape cji of each component isnormalized to unit area across the entire range of the CLUMPY wavelength grid0.011000 µm. We seek the optimal scale that minimize the error estimate function

χ2 =

Nλ∑i=1

(Mi − diσi

)2

(A.2)

of the composite SED. Evaluating all ∂χ2/∂Xj = 0 results in a general linear systemof equations (LSE)

Cx = d , (A.3)

where C is a symmetric Nc × Nc coecient matrix, d is a vector that contains theonly terms related to data uxes, and x is the sought-after vector of component scalesXj. In all generality Eq. (A.3) reads

∑i

c1i c

1i

σ2i

· · ·∑i

c1i cji

σ2i

· · ·∑i

c1i cNci

σ2i

... . . . ... . . . ...∑i

c1i cji

σ2i

· · ·∑i

cjicji

σ2i

· · ·∑i

cjicNci

σ2i

... . . . ... . . . ...∑i

c1i cNci

σ2i

· · ·∑i

cjicNci

σ2i

· · ·∑i

cNci cNciσ2i

X1

...

Xj

...

XNc

=

∑i

dic1i

σ2i

...∑i

dicji

σ2i

...∑i

dicNci

σ2i

. (A.4)

Given the data and the set of spectral shapes, all the sums in Eq. (A.4) are con-stants. The individual component scales Xj, j = 1, . . . , Nc can thus be obtainedanalytically, for instance by Gaussian elimination.

Depending on the spectral shapes of the data and the component SEDs, someof the scales can become negative. Mathematically the subtraction of a (scaled)

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component can lead to an overall better t, but this is of course not a physicalsolution. We are only interested in solutions that yield all scales non-negative. Thisis the case when the matrix C is positive-denite, i.e. when all of its eigenvalues arepositive. Then, since C is symmetric, a Cholesky decomposition C = LL

T exists, withL a lower triangular matrix and LT its transpose. The decomposition transforms thelinear system (A.3) into LLTx = d . Its solution is obtained through two simplerLSEs

L y = d ,

LTx = y ,

(A.5)

with y = LTx an auxiliary vector. This procedure requires only half the eort of the

Gaussian elimination. Adequate algorithms and their implementations are abundantin the literature (see, e.g., Press et al., 1996).

In our case with just two components, say A and B (for instance a torus and ablackbody component), the composite model SED is Mi = A · ai + B · bi, with A,B the yet unknown scales of the two components, and ai and bi their spectralshapes. Evaluation of Eq. (A.4) yields the two scales

A =1

S

(∑i

aidiσ2i

·∑i

b2i

σ2i

−∑i

bidiσ2i

·∑i

aibiσ2i

), (A.6)

B =1

S

(∑i

bidiσ2i

·∑i

a2i

σ2i

−∑i

aidiσ2i

·∑i

aibiσ2i

), (A.7)

with

S =∑i

a2i

σ2i

·∑i

b2i

σ2i

−(∑

i

aibiσ2i

)2

. (A.8)

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Appendix B

CLUMPY integration procedures

B.1 Integration in z-direction (1-D)

For any position (x, y) in the plane of the sky, and any given viewing angle i, andany wavelength λ, Clumpy performs an integration of the following function alongthe z-direction

Hλ(x, y; i) =

∫z

Pesc,λ(z′, z)Sc,λ(z

′)NC(z′) dz (B.1)

Figure B.1a shows an example brightness distribution in the xy-plane of the sky,with the proper names and values for the axes and area limits employed in Clumpy.

The integration path along z intersects the whole cloud distribution (at the given(x, y) position). Since there are no contributions to Eq. B.1 from regions outsidethe toroidal cloud distribution, the integration over dz practically begins at a point(x, y,−zmax) that corresponds to a radial distance of Ymax from the center, and endson the positive z-axis at a point (x, y, zmax) that fullls the same requirement. Fig-ure B.1b depicts an example of such integration along a path z towards the observer.

Under the z-integral in Eq. B.1 is a product of three functions. Each depends onz′, a location along the given z-path. The three function are:

• The local number of clouds per unit length NC(z′) at a position z′ along thez-path

• The intensity Sc,λ(z′) of a point source at z′

• The probability Pesc,λ(z′, z) of radiation generated at z′ to escape throughoutthe rest of the z-path without being absorbed by clouds

The intensity generated in a segment dz′ along the z-path is Sc,λ(z′)NC(z′) dz′.

The probability for the generated radiation to avoid all clouds throughout the restof the path is given in Natta and Panagia (1984) and in the appendix of Nenkovaet al. (2008a) by

Pesc,λ(z′, z) = e−tλ(z′,z) , (B.2)

where

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x

y

0−Ymax

Ymax

Ymax

x’

y’

(a)

z

1 Rd

Ymax

observer

(b)

Figure B.1: (a) Sample brightness distribution in the xy-plane of the sky. The areaof the calculational domain in Clumpy is contained within a rectangle with ver-tices (xmin, ymin, xmax, ymax) = (0,−Ymax, Ymax, Ymax). For any given position (x′, y′)Clumpy performs the z-integration given by Eq. B.1. (b) Vertical cut through atoroidal cloud distribution, illustrating integration along a particular path in the z-direction towards the observer. No integration is performed within the central cavityof 1Rd diameter (dashed part of the z path). For simplicity, a sharp-edged torus (inangular direction) is depicted, but generally smooth-edged tori are the rule.

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tλ(z′, z) = N (z′, z)

(1− e−τλ

), (B.3)

with τλ the dust optical depth for the given wavelength λ, and where

N (z′, z) =

∫ z

z′NC dz (B.4)

is the mean number of clouds between z′ and z. Written out, Pesc is

Pesc,λ(z′, z) = e

(∫ z

z′NC dz

) (1− e−τλ

)(B.5)

NC has units of inverse length (number of clouds per unit length), Pesc is a unitlessquantity (due to integrating NC over dz), and the intensities Sc,λ of the source pointsare given as uxes λFλ/FAGN , thus being a scaled, unitless quantity. The resultingintegral Hλ(x, y; i) from Eq. B.1 is therefore, like Sc,λ, a scaled and unitless quantityof type λFλ/FAGN .

B.2 Integration of brightness maps (2-D)

B.2.1 Goal

The spectral energy distribution (SED) to be outputted by Clumpy is basically thetotal ux emerging from the cloud distribution that is visible in the plane of the skyat each wavelength λ and for a given viewing angle i.

In order to calculate the SED, an area-integration of the individual point bright-nesses Hλ(x, y; i) from Eq. B.1 is necessary

ICλ (i) =

∫A

Hλ(x, y; i) dA , (B.6)

where A is the area over which the integration is performed. For Clumpy calcu-lations, A is conned by a 2D-rectangle with the vertices (xmin, ymin, xmax, ymax) =

(0,−Ymax, Ymax, Ymax), and Eq. B.6 can be written as

ICλ (i) =

∫y

∫x

Hλ(x, y; i) dx dy , (B.7)

with dA = dx dy. To calculate ICλ (i) Clumpy must perform a two-dimensionalintegration over the area in the plane of the sky that contains the given cloud distri-bution. Outside that cloud distribution, all contributions are zero, and thus need notbe calculated.

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B.2.2 Monte-Carlo methods

The simplest approach to achieve this 2D-integration would be to cover the rectangu-lar area with a rectilinear 2D-grid featuring some (not necessarily constant) spacings∆x, ∆y, then calculate Hλ(x, y; i) on the grid vertices according to Eq. B.1, and -nally simply Simpson-integrate the obtained point brightnesses using the known gridspacings ∆x, ∆y. However, this approach experiences two major drawbacks.

Firstly, since in general there is no a priori knowledge about the distribution ofbrightness within the area of integration, it is impossible to choose a suitable grid,one which is denser in regions of greater brightness variation, and coarser in regionswith at local brightness proles.

Secondly, and more importantly, this method does not allow for any kind of con-vergence checking of the obtained integration result. With a preset grid one can notbe sure at all whether the 2D integral really converged, or whether applying a nergrid would have changed the resultant integral signicantly.

One can give up the idea of a rectilinear grid, on whose vertices the integralB.1 is evaluated. A random (e.g. uniformly random) or quasi-random (e.g. Sobol'sequences) choice of points in the xy-plane would then yield a collection of pointbrightnesses, for which to integrate over the area one would employ Monte-Carlo in-tegration schemes (for deeper information on Monte-Carlo methods see for instancePress et al. (1996)). The book also explains in greater detail the adaptation necessarybetween successive iteration steps (see subroutines miser and vegas from NumericalRecipes). Aside from Numerical Recipes algorithms the CUBA library described insection B.2.3 also allows, together with its adaptive iteration schemes, for random orquasi-random generation of positions (x, y).

The Monte-Carlo approach has been tried with Clumpy, and although the quasi-random Sobol'-sequence generated points (x, y) yielded faster convergence for typicalClumpy cloud distributions, the Monte-Carlo approach proved quite dicult to ne-tune for it to yield a predictable convergence behavior. Often excessive iteration andadaptation was required in order to cover regions of greater brightness variation (or,depending on the applied method, regions of higher brightness values) sucientlydense, resulting in a great number of performed z-integrations, and thus unaccept-able computing times. The method does, however, allow for a deterministic controlof the required convergence accuracy.

Mainly for these eciency reasons Clumpy does not employ Monte-Carlo meth-ods, but instead utilizes an adaptive, deterministic grid algorithm with sub-regioncubature from the CUBA library (subroutine cuhre). See sec. B.2.3.

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B.2.3 Adaptive methods and the CUBA library

The goal for the 2D-integration of brightness has to be

• a self-sustained, iterative and adaptive integration scheme

• that at each iteration step renes the grid only locally where necessary (savingCPU time),

• that iterates until the integral value diers from the previous iteration at mostby a user-dened accuracy,

• and that does not require a priori knowledge about the distribution of brightnessin the xy-plane.

The open-source CUBA library1 for multi-dimensional integration of a user-writtenfunction provides just that. It was developed by Thomas Hahn (Hahn, 2005) of theMax-Planck Institute for Physics in Munich / Germany, and is published under theGNU Lesser General Public License (http://www.fsf.org/licensing/licenses/lgpl.html).

CUBA is written in C, but comes with bindings for FORTRAN as well, thus itssubroutines can be called from within any FORTRAN program directly. The libraryoers four dierent subroutines that all perform a multi-dimensional integration of auser-provided function. The four algorithms dier in their strategies and approacheson how to achieve convergence of the multi-dimensional integral. For Clumpy, sub-routine cuhre has proven most ecient.

cuhre provides a globally adaptive subdivision scheme, i.e. after every iterationstep it identies sub-regions with largest variance, and, if the desired accuracy hasnot been achieved yet, evaluates the integral on additional points within the sub-region of greatest error. The algorithm further employs a high-degree cubature rulefor the integral estimation in individual sub-regions. The degree of the cubature canbe chosen by the user, but for Clumpy degree 9 appears to represent a very goodbalance of accuracy and speed.

After every iteration steps cuhre combines the results from all sub-regions, de-termines the total error of the integral, and decides whether to proceed with moreiterations or not.

The working principle of is best visualized with an example. Fig. B.2 shows for aparticular Clumpy model the distribution of points (x, y) generated by cuhre in theClumpy integration area, as the algorithm continues to generate additional points

1http://www.feynarts.de/cuba/

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0 1 2 3 4 5x [Rd ]

4

2

0

2

4y

[Rd]

0.01 ∗Npoints

0 1 2 3 4 5x [Rd ]

0.05 ∗Npoints

0 1 2 3 4 5x [Rd ]

0.25 ∗Npoints

0 1 2 3 4 5x [Rd ]

1.00 ∗Npoints

Figure B.2: Adaptive 2D integration of brightness by subroutine cuhre. For a par-ticular Clumpy model with Y = 5Rd the pole-on view on Clumpy's calculationaldomain is shown (half-space due to symmetry). An accuracy of 1% on the integralconvergence was requested; a total number of npoints = 60,000 points in the xy-plane were necessary to achieve it. The four panels depict from left to right howCUBA's subroutine cuhre continued to adapt the grid locally and evaluated the in-tegral on additional points within rectangular sub-regions that show high variance.Particularly striking are two concentrations of points. Around and within 1Rd is theregion where the brightness varies the most due to highest dust temperatures andcloud number densities. The accumulation around Ymax results from the fact that thebrightness values beyond Ymax are numerically zero. This presents a somewhat sharpboundary that increases the local variance.

in order to achieve an accuracy of at least 1%.

B.2.4 Jacobian integral scaling

All CUBA subroutines operate strictly on a ndim-dimensional unit hypercube, withndim = 2 in the case of Clumpy (x and y axes). Thus all (x, y) positions generatedby CUBA are within the interval [0, 1] for both coordinates, and the area of integra-tion is a square. Clumpy on the other hand works within coordinates xc ∈ [0, Ymax]

and yc ∈ [−Ymax, Ymax]. The area of integration is rectangular, but certainly not theunit square. In order to make CUBA and Clumpy compatible, a mapping of (x, y)

coordinates generated by CUBA onto the coordinate space of Clumpy is required.This is accomplished by a coordinate transformation, which in turn leads to a scalingof the integral.

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Ac

ycmax

xcmax

ycmin

xminc

A1

0

y=1

x=1Figure B.3: Area transformation from the unit square area A1 to an arbitrary rectan-gular Clumpy integration area Ac. The boundary coordinates of Ac are given. Thetransformation consist of a translation and a homogeneous stretching along each axis.

We shall now derive in all generality a transformation from the unit square to anarbitrary rectangular area. Figure B.3 shows the unit square with area of integrationA1 and a possible Clumpy rectangular integration area Ac. The lower and upperboundaries of Ac shall be [xcmin, x

cmax] and [ycmin, y

cmax] for x

c and yc, respectively.

Calculus tells us, that a two-dimensional integral (in our case of a brightness functionI(x, y)) can be transformed from one integration domain into another like this∫∫

A1

I(x, y) dx dy =

∫∫Ac

I(xc, yc) det J dxc dyc , (B.8)

where J is the Jacobian matrix of the yet to be dened transformation

J =∂(x, y)

∂(xc, yc)=

∂x

∂xc∂x

∂yc

∂y

∂xc∂y

∂yc

. (B.9)

The transformation of the unit coordinates into another rectangular region is a simpletranslation plus homogeneous scaling. The new coordinates (xc, yc) are

xc = xcmin + x (xcmax − xcmin)

yc = ycmin + y (ycmax − ycmin)(B.10)

Solving for x and y, respectively, yields

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x =xc − xcminxcmax − xcmin

y =yc − ycminycmax − ycmin

.

(B.11)

We can now easily nd the determinant of the Jacobian matrix in Eq. (B.8), usingEq. (B.9) and (B.11), and bearing in mind that (x, y)c(min,max) are simply constants.

det J = det

∂x

∂xc∂x

∂yc

∂y

∂xc∂y

∂yc

=

∣∣∣∣∣∣1

xcmax−xcmin

0

0 1

ycmax−ycmin

∣∣∣∣∣∣=

1

xcmax − xcmin· 1

ycmax − ycmin− 0 =

1

∆xc ∆yc

(B.12)

Using the result of eq. (B.12) in eq. (B.8) we get∫∫A1

I(x, y) dx dy =1

∆xc ∆yc

∫∫Ac

I(xc, yc) dxc dyc , (B.13)

or equivalently

∆xc ∆yc∫∫A1

I(x, y) dx dy =

∫∫Ac

I(xc, yc) dxc dyc . (B.14)

Eq. (B.14) means that calculating the 2D brightness integral in Clumpy's domain(right hand side) is tantamount to calculating it on a unit square and then multiply-ing the result with the ranges of all dimensions of the Clumpy integration area (lefthand side). Thus the CUBA library and Clumpy are easily made compatible.

Any additional dimension xci , so long as coordinate-transformed in the fashion of eq.(B.10), would just add as a constant factor ∆xci on the left hand side of eq. (B.14).

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Appendix C

Kullback-Leibler Divergence

C.1 Denition

Given two probability density distributions (PDF), the Kullback-Leibler divergenceDKL can be used to measure the dierence between them. It is also called information

divergence, information gain, or relative entropy. In practical applications, like theBayesian inference in this work, one of the PDFs typically is the prior distribution of amodel parameter, while the other is the posterior. The dierence between these two,as measured by DKL, quanties how much information has been gained by introducingthe data. The formal denition follows below.

Let p(x), t(x) be prior and posterior probability density distributions of a contin-uous random variable x, such that∫

p(x) dx = 1,

∫t(x) dx = 1. (C.1)

The Kullback-Leibler divergence is

DKL =

∫t(x) ln

t(x)

p(x)dx. (C.2)

In other contexts DKL may have a dierent base than the natural logarithm. However,most expressions involving DKL hold irrespective of base.

C.2 Constant prior

Limit x to a closed interval [a, b] = x : a ≤ x ≤ b. If the prior is uniform, thenp(x) = 1/(b− a) ≡ 1/∆x.1 Insert this in (C.2)

DKL =

∫t(x) ln

t(x)

1/∆xdx =

∫t(x)

(ln t(x)− ln

1

∆x

)dx. (C.3)

Remember ∆x = const., and apply (C.1)

DKL =

∫t(x) ln t(x) dx− ln

1

∆x

∫t(x) dx (C.4)

=

∫t(x) ln t(x) dx− (ln 1− ln ∆x) (C.5)

=

∫t(x) ln t(x) dx+ ln ∆x (C.6)

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norm

aliz

ed p

rior

/ post

eri

or

a a' b' b

prior p(x)posterior t(x)

a=a' b' b

prior p(x)posterior t(x)

Figure C.1: Uniform prior (blue) and a piecewise-uniform posterior (red). By de-nition both are probability density functions, i.e. are normalized to unit area. Left:posterior constant on some sub-interval [a′, b′]. Right: w.l.o.g. that posterior alignedush left, i.e. a′ = a.

C.3 The meaning of DKL

C.3.1 (Piecewise) constant posterior

Assume the posterior is uniform, but subtends only some sub-range [a′, b′] = x : a′ ≤ x ≤ b′,such that a′ ≥ a and b′ ≤ b (see Figure C.1, left). The posterior is then dened as

t(x) =

0, x < a′

1/(b′ − a′) = 1/δx, a′ ≤ x ≤ b′

0, x > b′.

(C.7)

W.l.o.g. we can assume that the sub-range is aligned ush left within [a, b] (see Fig.C.1, right), such that a′ = a. Eq. (C.7) then reads

t(x) =

1/(b′ − a) = 1/δx, a ≤ x ≤ b′

0, b′ < x ≤ b.(C.8)

For DKL from (C.6) it then follows

DKL =

b∫a

t(x) ln t(x) dx + ln ∆x (C.9)

1Proof:

∫ b

a

p(x) dx =

∫ b

a

dx

∆x=

x

∆x

∣∣∣ba

=b

∆x− a

∆x=

b− a∆x

=∆x

∆x= 1, as required by Eq.

(C.1).

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=

b′∫a

1

δxln

1

δxdx +

b∫b′

0 · ln 0 dx

︸ ︷︷ ︸=0

+ ln ∆x (C.10)

With δx = const.

DKL =1

δxln

1

δx

b′∫a

dx + ln ∆x (C.11)

=1

δx(ln 1− ln δx) · x

∣∣∣b′a

+ ln ∆x (C.12)

=− ln δx

δx· (b′ − a)︸ ︷︷ ︸

=δx

+ ln ∆x (C.13)

= ln∆x

δx. (C.14)

It follows from (C.14) that

limδx→0

DKL =∞, and limδx→∆x

DKL = 0. (C.15)

Note that (C.14) holds even if the constant posterior is not contiguous, i.e. ifδx =

∑i δxi for a number of sub-ranges.

C.3.2 Gaussian posterior

We wish to be able to compare a non-at posterior with our at priors. What is themeaning of a given DKL value? Let us express DKL values for a Gaussian posteriorof some width. It's denition is

t(x) =1

σ√

2πe−

(x− µ)2

2σ2 . (C.16)

This Gaussian is always normalized to unit area, precisely what is needed for a prob-ability density function. W.l.o.g. we can assume a zero mean, i.e. µ = 0

t(x) =1

σ√

2πe−x2

2σ2 . (C.17)

To simplify the subsequent calculations, parametrize

a =1

σ√

2. (C.18)

Then Eq. (C.17) reads

t(x) =a√πe−a

2x2. (C.19)

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Use this in our previous expression (C.6) for DKL with a at prior

DKL =

∫t(x) ln t(x) dx + ln ∆x (C.20)

=

∫a√πe−a

2x2· ln

(a√πe−a

2x2)dx + ln ∆x (C.21)

Remember that ln is the natural logarithm

DKL =a√π

∫e−a

2x2(

lna√π

+ ln e−a2x2)dx + ln ∆x (C.22)

=a√π

lna√π

∫e−a

2x2dx︸ ︷︷ ︸

I1

− a3

√π

∫x2 e−a

2x2dx︸ ︷︷ ︸

I2

+ ln ∆x. (C.23)

From calculus (or integral tables, here from Bronstein et al. (2004)):∫ ∞0

e−a2x2

dx =

√π

2aand

∫ ∞0

x2e−a2x2

dx =

√π

4a3. (C.24)

Since both e−a2x2

and x2 e−a2x2

are even functions (symmetric w.r.t. x = 0)

I1 =

∫ ∞−∞

e−a2x2

dx = 2

∫ ∞0

e−a2x2

dx =

√π

a(C.25)

I2 =

∫ ∞−∞

x2e−a2x2

dx = 2

∫ ∞0

x2e−a2x2

dx =

√π

2a3. (C.26)

Use (C.25) and (C.26) in (C.23)

DKL =a√π

ln

(a√π

) √π

a− a3

√π

√π

2a3+ ln ∆x (C.27)

= ln

(a√π

)− 1

2+ ln ∆x. (C.28)

Re-use a = 1/(σ√

2) from (C.18)

DKL = ln1

σ√

2π− 1

2+ ln ∆x (C.29)

= ln 1 − lnσ√

2π − 1

2+ ln ∆x (C.30)

= ln∆x

σ√

2π− 1

2. (C.31)

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10-4 10-3 10-2 10-1 100

δx/∆x or σ/∆x

0

1

2

3

4

5

6

DKL

Kullback-Leibler divergence, assuming a flat prior

flat posterior of width δx

Gaussian posterior of width σ

Figure C.2: Kullback-Leibler divergence DKL given a at prior, and either a piecewiseat (red) or a Gaussian posterior (blue). The abscissa shows the width of bothposteriors in units of the full parameter interval ∆x. Note the upper limit for thewidth of the Gaussian at approx. 0.242 ∆x (dashed line; see Section C.4).

C.3.3 Results

Fig. C.2 shows the DKL values when the prior is at across the entire interval ∆x,and the posterior is either at across a sub-range δx (red), or a Gaussian of width σ(blue).

C.4 Limits

Both results (C.6) for a piecewise at posterior and (C.31) for a Gaussian posteriorset upper limits on the width of the posterior. For the piecewise at posterior

DKL = ln∆x

δx, (C.32)

and since DKL ≥ 0 always,

ln∆x

δx≥ 0 (C.33)

ln ∆x− ln δx ≥ 0 (C.34)

δx ≤ ∆x. (C.35)

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10 5 0 5 10x

0.00

0.05

0.10

0.15

0.20

0.25

0.30

0.35

0.40

pro

babili

ty d

ensi

ty f

unct

ion

maximal width of Gaussian posterior, assuming a flat prior

σ=1

σ=2

σ=3

Figure C.3: Maximal width of a Gaussian posterior, assuming a at prior.

unsurprisingly, the sub-range δx can not be larger than the full interval ∆x. For aGaussian posterior of width σ

DKL = ln∆x

σ√

2π− 1

2, (C.36)

and by the same argument

ln∆x

σ√

2π− 1

2≥ 0 (C.37)

∆x

σ√

2π≥ e1/2 (C.38)

σ ≤e−1/2

√2π

∆x ≈ 0.242 ∆x (C.39)

Therefore DKL is dened as long as the width σ of the Gaussian posterior does notexceed 24.2% of width of the parameter interval. But why? See Figure C.3.

C.5 Invariance under parameter transformations

The six Clumpy parameters are dened on very dierent value ranges. How does onecompare the DKL of such dierent parameters? A re-mapping of the x-coordinatesof any prior and posterior distributions to a common interval seems reasonable.

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a=0 1 b

dxdy

p(x)p(y)

Figure C.4: A linear transformation y(x) stretches a distribution function p(x) self-similarly, i.e. its relative shape is preserved. The area must remain one by denition.Therefore, p(x)dx = p(y)dy.

Dene a transformation y(x) which maps the x-interval [a, b] linearly onto the unitinterval [0, 1]

y(x) =x− ab− a

. (C.40)

Since p(x) dx = p(y) dy and t(x) dx = t(y) dy (see Figure C.4), Eq. (C.2) reads on aclosed interval [a, b]

DKL =

∫ b

a

t(x) lnt(x)

p(x)dx (C.41)

=

∫ y(b)

y(a)

t(y) lnt(y) dy

dx

p(y) dydx

dy (C.42)

=

∫ b−ab−a

a−ab−a

t(y) lnt(y)

p(y)dy (C.43)

=

∫ 1

0

t(y) lnt(y)

p(y)dy. (C.44)

Comparing (C.41) and (C.44) shows that the Kullback-Leibler divergence is invariantunder parameter transformations (not only the one used here). Therefore, the DKL

values of dierent parameters can be compared directly to each other; a re-mappingof coordinates is not necessary.

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VITA

Robert Nikutta

Date and place of birth

8 June 1976, Olsztyn / Poland

Educational institutions attended and degrees awarded

University of Kentucky, Lexington, Ph.D. in Astrophysics (2012)

Universität Potsdam (Germany), Diploma in Physics (2003)

Professional positions held

Research Assistant, University of Kentucky, 2006 - present

Teaching and Research Assistant, Universität Potsdam, 1999 - 2006

Professional Publications

Heymann, Nikutta, and Elitzur (2012, in prep.)

Nikutta, Asensio Ramos, Thompson, Heymann, and Elitzur (2012, in prep.)

Nikutta, Nenkova, Ivezi¢, and Elitzur (2012, in prep.)

Malmrose, Marscher, Jorstad, Nikutta, and Elitzur (2011a)

Malmrose, Marscher, Jorstad, Nikutta, and Elitzur (2011b)

Deo, Richards, Nikutta, Elitzur, Gallagher, Ivezi¢, and Hines (2011)

Nikutta, Elitzur, and Lacy (2009)

Nenkova, Sirocky, Nikutta, Ivezi¢, and Elitzur (2008b)

Votruba, Feldmeier, Kubát, and Nikutta (2008)

Votruba, Feldmeier, Kubát, and Nikutta (2007)

Feldmeier and Nikutta (2006)

112