29th International Symposium on Shock Waves 2

Riccardo Bonazza · Devesh RanjanEditors

29th International Symposiumon Shock Waves 2

ABC

EditorsRiccardo BonazzaDepartment of Engineering PhysicsUniversity of WisconsinMadisonUSA

Devesh RanjanDepartment of Mechanical EngineeringGeorgia Institute of TechnologyAtlanta, GAUSA

ISBN 978-3-319-16837-1 ISBN 978-3-319-16838-8 (eBook)DOI 10.1007/978-3-319-16838-8

Library of Congress Control Number: 2015934583

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5

Preface

The 29th International Symposium on Shock Waves (ISSW29) was held in Madi-son, WI, U.S.A., from July 14 to July 19, 2013. It was organized by the WisconsinShock Tube Laboratory, which is part of the College of Engineering of the Univer-sity of Wisconsin-Madison. The Organizing Committee consisted of Prof. RiccardoBonazza (conference chair), Prof. Devesh Ranjan (of Georgia Institute of Technol-ogy, conference co-chair), Prof. David Rothamer, and Dr. Jason Oakley. The Wis-consin Shock Tube Laboratory was established in 1998 with the dedication of itsunique facility: a 9.2 m long, vertical shock tube, with very large, square internalcross section, and structural capability for the firing of M=5 shock waves into at-mospheric air. Since the laboratory inception, the main focus of Prof. Bonazza’s re-search group has been the investigation of shock-accelerated inhomogeneous flows,with particular emphasis on the Richrmyer-Meshkov instability and the study ofshock-accelerated bubbles.

The International Symposium on Shock Waves originated in Boston in 1957 un-der the original name “International Symposium on Shock Tubes". The symposiaare held biennially and rotate among hosting countries all over the world. The Sym-posium had last been held in the U.S.A. in 2001, in Dallas Fort Worth, organized byProf. Frank Lu and his colleagues at the University of Texas at Arlington.

The venue for ISSW29 was the University of Wisconsin Memorial Union. TheMemorial Union building, located on the shore of Lake Mendota, was dedicated onOctober 5, 1928 and it offers UW students, faculty, staff, and the Madison com-munity spaces and facilities for a great variety of professional, educational, andsocial activities. All invited and contributed talks, poster sessions, lunches, and cof-fee breaks were held in the Memorial Union building. The building’s immediatesurroundings, especially “The Terrace", provided ideal places for quick break-outsand after-hour relaxation. There were 224 conference participants (80 of whom werestudent) and 14 participants in the companion program, all coming from 19 differentcountries.

At the time of the call for abstracts, 291 abstracts were submitted and sent outto 90 reviewers. The conference had 9 invited presentations, 220 contributed pre-sentations (divided into 70 parallel sessions, in 23 different areas), and 50 poster

VI Preface

presentations. The program was anchored by the Paul Vieille Lecture, presented onMonday morning by Prof. Gabi Ben-Dor of Ben-Gurion University of the Negev,with a talk on “Hysteresis phenomena in reflection of shock waves"; and by theKazuyoshi Takayama Lecture, established to celebrate the contributions to the fieldof shock waves science by Prof. Kazuyoshi Takayama. The Takayama Lecture waspresented on Friday afternoon by Prof. Beric Skews of the University of the Witwa-tersrand, with a talk on “Evolution of research - a case study".

ISSW29 had the largest number of Medical and Biological Applications talks(both invited and contributed) in the history of the ISSW, a testament to theformidable growth of this research area in the past few years, and to the tight con-nection the international shock wave community wants to maintain and foster withour colleagues in the medical field.

There were two student competitions, one for the best oral presentation andone for the best poster presentation, with awards ($500 for honorable mention and$1,000 for the winner) generously provided by the International Shock Waves Insti-tute. The student competition was first held in 2007 at ISSW26 in Göttingen. Whilethe format has varied over the years, the spirit of the competition and its awardsremains the same: to reward excellence among young scientists, and promote stu-dent growth and opportunities. For ISSW29, at the time of full paper submission,the authors were asked to indicate if they were participating in either competition.For the oral awards, there were 46 participants in 13 Student Competition oral ses-sions while the poster competition had 9 participants. Oral and poster presentationswere judged by a panel of evaluators and by the session chairs. To be eligible for theawards, the authors were required to be personally present at the conference. Thehonorable mention for the Student Oral Presentation Competition went to ShalanHooseria, of the Flow Research Unit, University of the Witwatersrand, Johannes-burg, for the paper “Three-dimensional Curved Shock Wave Interactions with Slen-der Bodies at Incidence". The winner of the Student Oral Presentation Competitionwas Wouter Mostert, of the School of Mechanical and Mining Engineering, Uni-versity of Queensland, for the paper “Characterisation of the Cylindrical RiemannProblem in Magnetohydrodynamics". The honorable mention of the Student PosterPresentation Competition went to Minghu Wang of the University of Science andTechnology of China, for the paper “Experimental study on interaction of planarshock wave with polygonal helium cylinder". The winner of the Student Poster Pre-sentation Competition was Keisuke Ouchi, of the Muroran Institute of Technology,for the paper “Numerical and experimental investigations of fluidic thrust vectoringwith oblique shock waves".

A new activity was held for the first time at ISSW29: a picnic strictly reservedto the students. The picnic was held at a city park within walking distance of theconference venue and hosted by UW-Madison graduate students. The intent was toprovide the students with an opportunity to meet and visit in a relaxed setting.

The traditional excursion on Wednesday took the conference participants tothe city of Milwaukee to visit the Harley-Davidson Museum and the MilwaukeeArt Museum. The Harley-Davidson Museum celebrates Wisconsin’s best knowbrand, with hundreds of motorcycles going back all the way to serial number 1.

Preface VII

The Milwaukee Art museum is home to a vast collection of paintings, sculptures,prints, drawings, decorative arts, and photographs on display at the magnificentQuadracci Pavilion designed by Spanish architect Santiago Calatrava.

The companion program took friends and families of the conference participantsthrough some of Madison’s most interesting sites and to two out-of-town attrac-tions: Taliesin, a collection of homes designed by Wisconsin native Frank LloydWright; and to the International Crane Foundation, a world-renown center for thepreservation of endangered species.

Meetings of the Shock Waves Editorial Board, the International Shock WavesInstitute Board, and the International Advisory Committee of the ISSW were heldduring the week. Traditionally, the IAC meeting is when the host of the next ISSWis selected. At ISSW29, a new format was established by selecting venues for thenext two ISSWs. This allows more time for the future conference hosts to developtheir conference plans, and organizational team. ISSW30 will be held in July 2015in Tel Aviv, Israel, and will be hosted by Prof. Gabi Ben-Dor and his colleagues.ISSW31 will be held in Nagoya, Japan, in July 2017, and will be hosted by Prof.Akihiro Sasoh and his colleagues.

The organizers of ISSW29 express their gratitude to Sandia National Laborato-ries for its generous financial support of ISSW29.

Madison Riccardo Bonazza, chairJuly 2013 Devesh Ranjan, co-chair

Contents

Volume 2

Part XI: Magnetohydrodynamics

Characterisation of the Cylindrical Riemann Problemin Magnetohydrodynamics . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 823W. Mostert, V. Wheatley, R. Samtaney

A Numerical Method for Self-similar Solutions in IdealMagnetohydrodynamics . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 829A. Alshaarawi, C. Frisby, R. Samtaney

Linear Simulations of the Cylindrical Richtmyer-Meshkov Instabilityin Hydrodynamics and MHD . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 835S. Gao, R. Samtaney

Part XII: Medical and Biological Applications

Micro-shock Wave Assisted Plant Transformation . . . . . . . . . . . . . . . . . . . 843Divya Prakash Gnanadhas, Akshay Datey, Dipshikha Chakravortty,Jagadeesh Gopalan

Laboratory Blast Testing Methodologies . . . . . . . . . . . . . . . . . . . . . . . . . . . 849C. Needham, G. Rule

Development of a Novel Shock Wave Catheter Ablation System . . . . . . . . 855H. Yamamoto, Yuhi Hasebe, Masateru Kondo, Koji Fukuda,Kazuyoshi Takayama, Hiroaki Shimokawa

X Contents Volume 2

Underwater-Shock/Bubble Interaction and Its Application to Biologyand Medicine . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 861Kazuyoshi Takayama, H. Yamamoto, A. Abe

Uncovering the Secret of Shock Wave Lithotripsy . . . . . . . . . . . . . . . . . . . 869P. Zhong

Development of DDS Capsules Including Gas Bubblesby Shock Waves and Their Applications . . . . . . . . . . . . . . . . . . . . . . . . . . . 871Masaaki Tamagawa, Kenshi Morimoto, Koji Yagyu

DNA Integrity and Shock Wave Transformation Efficiency of Bacteriaand Fungi . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 873Achim M. Loske, Juan Campos-Gullén, Francisco Fernández,Xóchitl Pastrana, Denis Magaña-Ortíz, Nancy Coconi-Linares,Elizabeth Ortíz-Vásquez, Miguel Gómez-Lim

Biological Effects of Shock Waves on Infection . . . . . . . . . . . . . . . . . . . . . . 877Divya Prakash Gnanadhas, S. Janardhanraj,Dipshikha Chakravortty, Jagadeesh Gopalan

A New Biolistic Intradermal Injector Based on a Miniature ShockTube . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 883M. Brouillette

Translational Research for Blast-Induced Traumatic Brain Injury:Injury Mechanism to Development of Medical Instruments . . . . . . . . . . . 889A. Nakagawa, K. Ohtani, T. Arafune, T. Washio,M. Iwasaki, T. Endo, Y. Ogawa, T. Kumabe,K. Takayama, T. Tominaga

Shock Waves for Possible Application in Regenerative Medicine . . . . . . . 893S.H.R. Hosseini, S. Moosavi Nejad, H. Akiyama

Development of Extracorporeal Shock Wave Therapy for theTreatment for Ischemic Cardiovascular Diseases . . . . . . . . . . . . . . . . . . . . 895Hiroaki Shimokawa

Visualization of Cell Membrane Poration by Microbubble Oscillation . . . 897S. Moosavi-Nejad, K. Tachibana, H. Akiyama, S.H.R. Hosseini

Part XIII: Nozzle Flow

Vortical Structures as Mach Wave Sources in the Mixing Layer ofSupersonic Jets . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 901H. Oertel, F. Seiler, J. Srulijes, Robert Hruschka

Contents Volume 2 XI

Mixing in a Supersonic Ejector - An Experimental Investigation . . . . . . . 907M.V. Srisha Rao, G. Jagadeesh

Coaxial Jets Entering into a Hot Environment . . . . . . . . . . . . . . . . . . . . . . 913I. Klioutchnikov, Herbert Olivier, J. Odenthal

Modification of Shock Train Induced Turbulence bya Variable Nozzle Opening Angle and CircumferentialSuction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 919A. Grzona, Alexander Weiss, Herbert Olivier

Part XIV: Numerical Methods

Effect of Flux Evaluation Schemes in Numerical Simulation ofShockwave-Gas Cylinder Interaction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 927M.P. Ray, B.P. Puranik, U.V. Bhandarkar

Low Mach Number Effect in Simulation of High Mach Number Flow . . . 933X.Y. Hu, N.A. Adams

Particle-Based Simulation of Shock-Induced Deformation of ElasticBodies . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 939Y. Sakamura, T. Sugimoto, K. Nakayama

Parallel Anisotropic Block-Based Adaptive Mesh Refinement Schemefor the Study of Oblique Shock Reflections . . . . . . . . . . . . . . . . . . . . . . . . . 945M.K. Hryniewicki, C.P.T. Groth, J.J. Gottlieb

A Hierarchical WENO Reconstructed Discontinuous GalerkinMethod for Computing Shock Waves . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 951Y. Xia, M. Frisbey, H. Luo

Part XV: Plasmas

Return Stroke with Current behind the Shock Front . . . . . . . . . . . . . . . . . 959M. Hemmati, W. Childs, H. Morris, H. Shojaei, P. Pinkston

Interaction of Laser Induced Micro-Shockwaves . . . . . . . . . . . . . . . . . . . . 965Ch. Leela, Suman Bagchi, Surya P. Tewari, P. Prem Kiran

Ionization Front and Shock Wave Structures in MicrowavePropulsion . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 971M. Takahashi, H. Miyamoto, Y. Okuno, N. Ohnishi

XII Contents Volume 2

Part XVI: Propulsion

Influence of Gaseous Contaminations on Performance and Operabilityof a Scramjet Inlet . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 979Kunwei Liu, Yujian Zhu, Wenzhi Gao, Jiming Yang

Experimental and Computational Study of Flow Interactions in aGeneric Scramjet Inlet-Isolator . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 985A. Che Idris, M.R. Saad, H. Zare-Behtash, K. Kontis

Performance Predictions of Supersonic Intakes withIsentropic-Compression Forebody . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 991K. Nakashima, Tsutomu Saito

Numerical Investigation of the Mixing Process in Inlet-fuelledScramjets . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 997R.M. Gehre, D. Peterson, V. Wheatley, R.R. Boyce

Experimental Investigation of a Hypersonic Inlet with VariableSidewall for Flow Control . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1003T.C. Rolim, F.K. Lu

Ground Based Testing and Numerical Studies of aLarge Axisymmetric Scramjet Engine in the HIEST TestFacility . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1009D. Oberg, R.R. Boyce, L. Brown, K. Itoh, T. Komuro

Numerical and Experimental Investigations of Fluidic ThrustVectoring with Oblique Shock Waves . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1015K. Ouchi, K. Yamada, M. Hirota, Kazuaki Hatanaka,Tsutomu Saito, L. Li

Gas Flow in Ejector of Pulse Detonation Engine . . . . . . . . . . . . . . . . . . . . . 1021A. Korobov, S.V. Golovastov, V.V. Golub

On the Self-starting Constraints for Busemann Intakes withOverboard Spillage . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1027N. Moradian, E.V. Timofeev, R. Tahir, S. Mölder

Part XVII: Richtmyer-Meshkov Instability

Experimental Study of the Richtmyer-Meshkov Instability Inducedby Cylindrical Converging Shock Waves . . . . . . . . . . . . . . . . . . . . . . . . . . . 1035Ting Si, Zhigang Zhai, Xisheng Luo, Jiming Yang

Contents Volume 2 XIII

Comparative Study of the Predictions of FourReynolds-Averaged Navier–Stokes Turbulence Models Applied to aRichtmyer–Meshkov Instability Experiment . . . . . . . . . . . . . . . . . . . . . . . . 1041Oleg Schilling

Reynolds-Averaged Navier–Stokes Modeling of ReshockedRichtmyer–Meshkov Instability Experiments and Simulations . . . . . . . . . 1047J. Tiberius Morán-López, Oleg Schilling, James P. Holloway

On the Evolution of Reshocked Gas Cylinder Under Planar andConverging Shock Conditions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1053Zhigang Zhai, Ting Si, Xisheng Luo, Jiming Yang

Experimental Study on the Interaction of Planar Shock Wave withSquare Helium Cylinder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1059Minghu Wang, Ting Si, Xisheng Luo

Generation of Air/SF6 Interface with Minimum Surface Feature bySoap Film Technique . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1065Xiansheng Wang, Ting Si, Xisheng Luo, Jiming Yang

Richtmyer-Meshkov Instability of a Multimode Interface Acceleratedby a Toroidal Shock Wave . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1071Tong Long, Ting Si, Xisheng Luo

Generation of Cylindrical Converging Shock Waves in a ConventionalShock Tube . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1077L. Biamino, G. Jourdan, C. Mariani, L. Houas,M. Vandenboomgaerde, D. Souffland

Experimental Determination of the Growth Rateof Richtmyer-Meshkov Induced Turbulent Mixing afterReshock . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1083G. Bouzgarrou, Y. Bury, S. Jamme, L. Joly, J.-F. Haas

Richtmyer-Meshkov Instability of the Explosive Heavy Gas Cloud . . . . . 1089Dawen Xue, Zhihua Chen, Xiaohai Jiang

Investigating the Multi-layered Richtmyer-Meshkov Instabilitywith High-Order Accurate Numerical Methods . . . . . . . . . . . . . . . . . . . . . 1095Marc T. Henry de Frahan, Pooya Movahed, Eric Johnsen

Investigation of Mach Number Dependence on theRichtmyer-Meshkov Mixing Transition for a ShockedHeavy-Gas Curtain . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1101G. Orlicz, S. Balasubramanian, K. Prestridge

XIV Contents Volume 2

The Magnetohydrodynamic Richtmyer-Meshkov Instability: TheOblique Field Case . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1107V. Wheatley, R.M. Gehre, R. Samtaney, D.I. Pullin

Numerical Simulations of the Chemically Reacting Single-ModeRichtmyer-Meshkov Instability . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1113N. Attal, P. Ramaprabhu

Large Amplitude Nonlinear Richtmyer-Meshkov Instability inConvergent Geometries . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1119A. Nelson, P. Ramaprabhu

Simultaneous PIV and PLIF Measurements of Mach Number Effectson Single-Interface Richtmyer-Meshkov Mixing . . . . . . . . . . . . . . . . . . . . . 1125B.M. Wilson, R. Mejia-Alvarez, K. Prestridge

Richtmyer-Meshkov Instability at Solid-gas Interfaces . . . . . . . . . . . . . . . 1131A. López Ortega, M. Lombardini, P.T. Barton, D.I. Pullin,D.I. Meiron

Experimental Study of Turbulent Mixing in the Richtmyer-MeshkovInstability . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1137C. Weber, N. Haehn, J. Oakley, D. Rothamer, R. Bonazza

An Experimental Study of the Turbulent Developmentof Richtmyer-Meshkov Instability from a Three-DimensionalRandom Initial Perturbation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1143V. Tsiklashvili, O.A. Likhachev, J.W. Jacobs

Experiments on the Expansion Wave DrivenRayleigh-Taylor Instability . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1149R.V. Morgan, O.A. Likhachev, J.W. Jacobs

Simultaneous PIV/PLIF Measurements ofMulti-mode Perturbed Initial Conditions ofSingle-Interface Richtmyer-Meshkov Mixing . . . . . . . . . . . . . . . . . . . . . . . 1155R. Mejia-Alvarez, B.M. Wilson, K. Prestridge

Simulations and Experimental Investigation of the Inclined InterfaceRichtmyer-Meshkov Instability . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1161Jacob A. McFarland, Skylar Creel, Thomas Finn,Christopher McDonald, David Reilly, Jeffrey Greenough,Devesh Ranjan

Inclined Interface Richtmyer-Meshkov Instability: Reshock Study . . . . . 1167Skylar Creel, Jacob A. McFarland, Thomas Finn,Christopher McDonald, David Reilly, Jeffrey Greenough,Devesh Ranjan

Contents Volume 2 XV

Part XVIII: Shock-Boundary Layer Interaction

Experimental Study of Dual Injections with a Cavity in SupersonicFlow . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1175T. Ukai, H. Zare-Behtash, K.H. Lo, K. Kontis, S. Obayashi

Incident Shock-Transverse Jet Interactions at Mach 1.9: Effect ofShock Impingement Location . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1181H. Zare-Behtash, K.H. Lo, E. Erdem, K. Kontis, J. Lin, T. Ukai,S. Obayashi

Incident Shock-Transverse Jet Interactions at Mach 1.9: Effect ofDifferent Jet Gases . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1187J. Lin, H. Zare-Behtash, K.H. Lo, E. Erdem, K. Kontis

Numerical Study on Shock Wave Interaction over CompressionCorner with 30 deg. in Hypersonic Flow . . . . . . . . . . . . . . . . . . . . . . . . . . . 1193T. Kuramoto, D. Muto, N. Tsuboi, H. Nagai, Keisuke Asai

Experimental Investigation of Axisymmetric Transitional Shock WaveBoundary Layer Interactions at Mach 5 . . . . . . . . . . . . . . . . . . . . . . . . . . . 1199E. Erdem, K. Kontis, E. Johnstone, N. Murray, J. Steelant

Analysis of 2D Shock-Wave/Boundary-Layer Interaction Phenomena . . . 1205M. Bordbar, Y.F. Yao

Experimental Study of Supersonic Flow over a Forward Facing Step . . . 1211M. Jayaprakash Narayan, Raghuraman N. Govardhan

Shock Tunnel Investigations on Impinging Shock Wave BoundaryLayer Interactions at Hypersonic Speeds . . . . . . . . . . . . . . . . . . . . . . . . . . . 1217R. Sriram, Mohammed Ibrahim, G. Jagadeesh, K.P.J. Reddy

Numerical Predictions of Influence of Boundary Layer onHemispherical Imploding Shock Focusing . . . . . . . . . . . . . . . . . . . . . . . . . . 1223Tsutomu Saito, Kazuaki Hatanaka, Kazuyoshi Takayama

Micro-Ramps Flow Characteristics at Mach 1.9 & 5 . . . . . . . . . . . . . . . . . 1229M.R. Saad, A. Che Idris, K.H. Lo, K. Kontis

Modelling Shock Wave/Boundary Layer Interactions Using AdvancedRANS Models . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1235I. Asproulias, A.J. Revell, T.J. Craft

XVI Contents Volume 2

Unsteady Shock Motion in a Transonic Flow over a Wall-MountedHemisphere . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1241Steven J. Beresh, John F. Henfling, Russell W. Spillers,Brian O.M. Pruett

Experimental Study of Effect of Jets Injected into Supersonic MainFlow on Porous Cavity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1247N. Kuniyoshi, M. Yaga, I. Teruya, M. Ishikawa

Control of Shock Unsteadiness in a Cylindrical Protuberance InducedInteraction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1253P. Akshara, C. Mani Sankar, S.B. Verma

Effect of the Rotation of Finned Projectiles on Drag and BasePressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1259Robert Hruschka, Friedrich Leopold

Numerical Prediction of 3-D Supersonic Turbulent SeparationInitiated by a Single-Fin . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1265A. Salin, Y.F. Yao, A.A. Zheltovodov

Part XIX: Shock Propagation and Reflection

Attenuating Shock Waves by Barrier Having Different Orientations:A Numerical Investigation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1273D. Igra, O. Igra

Shock Wave Diffraction at the Inclined Exitof a Shock Tube . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1279R.T. Paton, B.W. Skews

Effect of Wedge Bluntness on Oblique Shock Reflection . . . . . . . . . . . . . . 1285S. Kobayashi, T. Adachi

Three-Dimensional, Curved Shock Wave Interactions with SlenderBodies at Incidence . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1291S.J. Hooseria, B.W. Skews

Numerical Simulation and Experiments on the Ground Effect ofTransonic Projectiles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1297J. Young, K. Carriage, B. Oakes, H. Kleine, K. Hiraki, Y. Inatani

A Summary of Shock/Soap Bubble Interactions Performed at theSWRC, Tohoku University . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1303H. Yamamoto, D. Igra, Kazuyoshi Takayama

Contents Volume 2 XVII

Experimental Investigation into Converging Cylindrical Shock WaveReflection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1309B.J. Gray, B.W. Skews

Onset of Shear Layer Instability in Shock Diffraction Processes . . . . . . . . 1315H. Kleine, I. Klioutchnikov, H. Olivier

Cumulation Effects for Interaction of a Shock with Elliptic GasBubbles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1321P. Georgievskiy, V.A. Levin, O. Sutyrin

On the Influence of Reynolds Number on the Mach Stem Height atShock Reflection from a Circular Cylinder . . . . . . . . . . . . . . . . . . . . . . . . . 1327E.V. Timofeev, A. Hakkaki-Fard, H. Kleine, B.W. Skews

Numerical Study of Flow Structure Near Triple Shock WaveIntersection in Steady Flows . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1333G. Shoev, D. Khotyanovsky, Y. Bondar, A. Kudryavtsev,M.S. Ivanov

Interaction between Underwater Explosion and Porous Foam Layer . . . . 1337K. Kitagawa, A. Abe, K. Ohtani

Characterization of a High Temporal Resolution TDLAS System forMeasurements in a Shock Tube Facility . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1343F. Förster, Sean O’Byrne, H. Kleine, B. Weigand

Emitting Shock Waves by a Laser Driven Collapsing Bubble inGlycerine and Water . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1349W. Garen, F. Hegedüs, S. Koch, B. Meyerer, W. Neu, U. Teubner

Consideration of the Effect of Length-Scale Information on Regularto Mach Reflection Transition in the Presence of Dynamic Effects . . . . . . 1355K. Naidoo, B.W. Skews

Shock Wave Focusing in a Concave Profile . . . . . . . . . . . . . . . . . . . . . . . . . 1361D.A. MacLucas, B.W. Skews, H. Kleine

Specific Features of Shock Wave Refectionin Unsteady Flow . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1367I.V. Krassovskaya, M.K. Berezkina

On the Unsteady Shock Wave Interaction with a Backward-FacingStep: Viscous Analysis . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1373N. Mendoza, R.D.W. Bowersox

On the Unsteady Shock Wave Interaction with a Splitter Plate:Viscous Analysis . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1379N. Mendoza, R.D.W. Bowersox

XVIII Contents Volume 2

On the Transition from Regular to Mach Reflection in OverexpandedPlanar Jets . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1385E. Shimshi, G. Ben-Dor, A. Levy

Part XX: Shock-Vortex Interaction

Two-Point Measurements of Post-shock Overpressure Past a GridTurbulence . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1393T. Harasaki, T. Kitamura, Akihiro Sasoh, K. Nagata, Y. Sakai

Control of Flow Separation on a Contour Bump by Jets: AnExperimental Study . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1399K.H. Lo, H. Zare-Behtash, M. Johnson, K. Kontis

Large Deformation of Bow Shock Waves Ahead of a Forward-FacingHemisphere . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1405Toshiharu Mizukaki, Kazuaki Hatanaka, Tsutomu Saito

Laser Energy Deposition for Shock Wave Boundary Layer Control atSupersonic Speeds . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1411E. Erdem, K. Kontis, T. Osuka, R. Majima, T. Tamba, Akihiro Sasoh

The Effect of the Recombination Shock behind a Backward Step onthe Mixing Characteristics of an Inclined Sonic Methane Jet in aSupersonic Crossflow . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1417A.C.Y. Wen, B.Y.C. Chang, C.Y.H. Su, D.H.F. Yuan

Direct Numerical Simulations of Isotropic Turbulence Interactingwith a Shock Wave . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1423Jaiyoung Ryu, Daniel Livescu

Part XXI: Shock Waves in Condensed Matter

Oxidation Resistance Studies of Silicon Carbide Thin Film in a FreePiston-Driven Shock Tube . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1431N. Thanganayaki, K.P.J. Reddy, V. Jayaram

Structure of Shock Waves in Complex Molecular Liquids . . . . . . . . . . . . . 1437Z.A. Walenta, A.M. Slowicka

Contents Volume 2 XIX

Part XXII: Shock Waves in Multiphase Flow

Observation and Analysis of Microbubble Motion Induced by anUnderwater Shock Wave . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1445S. Maeno, J. Wang, S. Fukuda, A. Abe

Flash X-Ray Measurements during Shock Wave Interactions withDense Particle Fields . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1451J. Wagner, S. Kearney, Steven J. Beresh, Brian O.M. Pruett

Experimental Study of the Shock-Induced Acceleration and Breakupof Liquid Droplets . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1457Yi Xiao, Hong-hui Shi, Wu Yu, Chao Wang, Li-te Zhang,Ruo-ling Dong

Study on Supercavitating Flows Induced by Horizontally LaunchedProjectiles . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1463S.Y. Zhou, Hong-hui Shi, J.H. Hu, Q.Q. Hu, H.X. Jia, B. Chen

Modeling Environmental Effects of Pollutants Dispersion Generatedby Explosions in Confined Enclosures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1469Y. Lefler, D. Sidilkover, S. Pistinner

Wave-Induced Droplet Growth Measurementby Laser Light . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1475M. Fransen, E. Sachteleben, D. Smeulders

Shock Interactions with Dusty Gases . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1481M.G. Omang, J. Trulsen

Experimental Investigation of Shock-Wave Propagation in AqueousFoam . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1487G. Jourdan, C. Mariani, L. Houas, E. Del Prete, A. Chinnayya,A. Hadjadj, J.-F. Haas, N. Rambert, D. Counilh, S. Faure

Two-Dimensional Experiment on the Jet Formation during Dispersalof Solid Particles by Shock Wave . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1493V. Rodriguez, G. Jourdan, C. Mariani, R. Saurel, J.-C. Loraud,L. Houas, E. Lapébie, L. Munier, A. Osmont

Experimental and Numerical Investigation of the Propagation of aPlanar Shock Wave into a Cloud of Droplets . . . . . . . . . . . . . . . . . . . . . . . . 1499A. Chauvin, G. Jourdan, L. Biamino, E. Daniel, L. Houas,R. Tosello, D. Leriche

XX Contents Volume 2

Experimental Study of Underwater Shock Wave and CavitationGenerated by Underwater Electric Discharge in a Narrow Container . . . 1505T. Koita, K. Hayashi, Mingyu Sun

Numerical Modelling of Shock-Wave Propagation in a Shock TubeFilled with Aqueous Foam . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1511D. Counilh, E. Del Prete, A. Chinnayya, A. Hadjadj, N. Rambert,J.-F. Haas, G. Jourdan, C. Mariani, L. Houas

About Some Features of a Magma Flow Structure at ExplosiveVolcano Eruptions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1517V. Kedrinskiy

A New Facility for Studying Shock-Wave Passage Over Dust Layers . . . . 1523B. Marks, A. Chowdhury, E.L. Petersen, M.S. Mannan

Two-Dimensional Underwater Explosion Near a SurfaceStructure Predicted by a Numerical MultiphaseFlow Model . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1529G.S. Yeom, K.S. Chang

The Effects of Shock Strength on Droplet Breakup . . . . . . . . . . . . . . . . . . 1535Jomela C. Meng, Tim Colonius

A Simple Constitutive Model for Predicting the Pressure HistoriesDeveloped Behind Rigid Porous Samples Impinged by Shock Waves . . . . 1541O. Sadot, O. Ram, G. Ben-Dor, A. Levy, G. Golan,E. Ran, F. Aizik

A Conservative and Entropy-Nondecreasing Subgrid Closure Modelfor Two Compressible Materials in a Grid Cell . . . . . . . . . . . . . . . . . . . . . . 1547Mingyu Sun

Experimental Studies of Shock Interactions with a MultiphaseMedium . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1553C. Corbin, P. Vorobieff, P. Wayne, T. Bernard, C.R. Truman,S. Kumar

Part XXIII: Shock Waves in Rarefied Flow

The Analysis of Underexpanded Jet Flows for HypersonicAerodynamic Experiments in Vacuum Chambers . . . . . . . . . . . . . . . . . . . 1561V.V. Riabov, A.I. Fedoseyev

Diffraction of an Expansion Wave around a 90◦ Corner . . . . . . . . . . . . . . 1567I. Mahomed, B.W. Skews

Contents Volume 2 XXI

Vortex Shedding over a Discontinuous Edge . . . . . . . . . . . . . . . . . . . . . . . . 1573S. Cooppan, B.W. Skews

Kelvin-Helmholtz Instability on the Mach Reflection Shear Layer . . . . . . 1579S.R. Rubidge, B.W. Skews, R.T. Paton, I. Znamenskaya, I. Ivanov,I. Kryukov

Interaction between Shock Waves in Water and ConvergentStructures of Finite Thickness . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1585Chao Wang, Veronica Eliasson

A Hybrid MD-DSMC Algorithm to Model Wall Effects in aMicro-scale Shock Tube . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1591D.S. Watvisave, B.P. Puranik, U.V. Bhandarkar

About the Nature of Nonequilibrium Radiation of I2 in the Front of aShock Wave . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1597A. Emelianov, A. Eremin, S. Kulikov

A Numerical Solution of the Boltzmann Equation for the Shock WaveStructure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1603E.A. Malkov, M.S. Ivanov

Generation of Shock Wave by Temperature Change at Wall-2 . . . . . . . . . 1609M. Tsukamoto, A. Sakurai

Shock Transition Solutions of Navier-Stokes Equations with VolumeViscosity for Nitrogen and Air . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1615M.K. Hryniewicki, J.J. Gottlieb, C.P.T. Groth

Author Index . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1621

Keyword Index . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1629

Contents

Volume 1

Part I: Plenary Lectures

Hysteresis Phenomena in Reflection of Shock Waves . . . . . . . . . . . . . . . . . 3G. Ben-Dor

Ten Years of Shock Tube Research at Marseille . . . . . . . . . . . . . . . . . . . . . 11L. Houas

Driving Forward Innovation in High Speed Aerodynamics and FlowDiagnostics . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19Konstantinos Kontis

High-Speed Visualization of Compressible Flows – Potentialand Limitations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 27H. Kleine

Vortex Generation by Shock-Bubble Interaction in Galaxy Clusters . . . . 35S. Heinz, S. Friedman, E. Churazov

Vorticity and Vortex Models in Shock Accelerated GasInhomogeneities . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 43J.W. Jacobs

Successful Development of the Long-Test-Duration HypervelocityDetonation-Driven Shock Tunnel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 51Z.L. Jiang, H.R. Yu

Shock Waves in Relaxing Condensed Media . . . . . . . . . . . . . . . . . . . . . . . . 59G.I. Kanel

XXIV Contents Volume 1

Evolution of Research – A Case Study . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 67Beric Skews

Part II: Blast Waves

Laser-Induced Blast Waves in Air and Their Effect on MonodisperseDroplet Chains of Ethanol and Kerosene . . . . . . . . . . . . . . . . . . . . . . . . . . . 77G.C. Gebel, T. Mosbach, W. Meier, M. Aigner

Shock Tube Simulation of Low Mach Number Blast Waves . . . . . . . . . . . 83R.G. Morgan, D.E. Gildfind

Development of a Liquid Blast Tube Facility for Material Testing . . . . . . 89I. Obed Samuelraj, G. Jagadeesh

Analytical Solutions for the Point Source Spherical Blast WavePropagation with γ = 7 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 95Shuji Takahashi

Explosively-Driven Blast Waves in Small-Diameter Tubes . . . . . . . . . . . . . 101M.A. Cooper, R.T. Marinis, M.S. Oliver

Study on Excessive Pressure of Underwater Shock Wave Generatedin Confined Space . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 107H. Ueda, A. Abe

Time Evolution of the Density Field of a Micro–Explosion UsingBackground Oriented Schlieren . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 113P. Suriyanarayanan, L. Venkatakrishnan, G. Jagadeesh

Energy Analysis of a Small-Scale Combustion Driven Blast Tube . . . . . . . 119S. Janardhanraj, G. Jagadeesh

Shock Interaction Studies on Glass Fibre Reinforced Epoxy MatrixComposites . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 127K.P.J. Reddy, G. Jagadeesh, V. Jayaram, B. Harinath Reddy, V. Madhu,C. Jaya Rami Reddy

High Energy Concentration by Spherical Converging Shocksin a Shock Tube with Conically Shaped Test Section . . . . . . . . . . . . . . . . . 135N. Apazidis, M. Kjellander, N. Tillmark

A Pulsed Detonation Microthruster for Space Applications . . . . . . . . . . . . 141E. Martel, M. Brouillette

Contents Volume 1 XXV

Part III: Chemically Reactive Flows

Constrained Reaction Volume: A New Approach to Studying ReactiveSystems in Shock Tubes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 149R.K. Hanson, S. Chakraborty, G.A. Pang, W. Ren, S. Wang, D.F. Davidson

Laser Absorption Diagnostics for Aldehydes in Shock Tube KineticsStudies . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 155S. Wang, D.F. Davidson, R.K. Hanson

Electronic Excitation Modeling in Chemically Reacting HypersonicFlows . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 161V.A. Istomin, E.V. Kustova

Thermochemical Non-equilibrium Effects on Type VI-V Transitionin Hypersonic Double-Wedge Flow . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 167J. Li, Yujian Zhu, Xisheng Luo

A Computationally Efficient Approach to Hypersonic ReactingFlows . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 173J. Rabinovitch, G. Blanquart

Thermal Decomposition Study of 3-Carene . . . . . . . . . . . . . . . . . . . . . . . . . 179N. Sharath, K.P.J. Reddy, E. Arunan

Experimental Investigation of Propargyl Alcohol Pyrolysis . . . . . . . . . . . . 185N. Sharath, K.P.J. Reddy, E. Arunan

Shock Tube Studies on Thermal Decompositionof 2-Chloroethylbenzene . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 191M. Kiran Singh, K.P.J. Reddy, E. Arunan

Sensitivity of Shock-Tube Chemiluminescence Measurementsto the Optical Setup . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 197M.L. Davis, E.L. Petersen

Thermochemical Nonequilibrium Analysis of Oxygenin Shock Tube Flows . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 203Kevin Neitzel, Jae Gang Kim, Iain D. Boyd

Detailed Simulations of Weak-to-Strong Ignition of a H2/O2/ArMixture in Shock-Tubes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 209Matthias Ihme, Yong Sun, Ralf Deiterding

XXVI Contents Volume 1

Experimental Study of Intense Radiation around Si-BasedHeat-Resistant Materials in Air Plasma Freejets . . . . . . . . . . . . . . . . . . . . 215M. Funatsu, M. Ozawa, R. Onozawa, K. Konishi, M. Kawada,F. Takakusagi

Laser Absorption Measurements of CO at Elevated Pressuresbehind Reflected Shock Waves . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 221A. Camou, J.E. Vivanco, D.M. Cusano, E.L. Petersen

Numerical Study on the Heat Release Distributions of a SupersonicCombustor with Three-Dimensional “Swallowtail” Cavity . . . . . . . . . . . . 227Chun Wang, Xiaofeng Sun, Xuanyu Yao, Zonglin Jiang

Thermal Decomposition of Ethyl Formate behind the Reflected ShockWaves in the Temperature Range of 909-1258K . . . . . . . . . . . . . . . . . . . . . 233M. Balaganesh, G. Sudhakar, B. Rajakumar

Kinetics of the Thermal Decomposition of Tetramethylsilane behindthe Reflected Shock Waves in a Single Pulse Shock Tube (SPST) andModeling Study . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 239A. Parandaman, G. Sudhakar, B. Rajakumar

Part IV: Detonation and Combustion

Numerical Simulation of Aluminum Dust Detonations with DifferentProduct Phases . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 247H.H. Teng, Z.L. Jiang

Effect of Smoked Foil Thickness and Location on DetonationInitiation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 253K.M. Chung, C.S. Wen

Mid-infrared Laser Absorption Diagnostics for Detonation Studies . . . . . 259R.M. Spearrin, C.S. Goldenstein, J.B. Jeffries, R.K. Hanson

Shock Wave – Boundary Layer Interaction in Reactive H2/O2Mixture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 265E. Dzieminska, A.K. Hayashi

Propagation of Sinusoidally-Corrugated Shock Fronts ofLaser-Supported Detonations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 271T. Honda, A. Kawaguchi, Y. Hanta, A. Susa, S. Namba, T. Johzaki,T. Endo, H. Shiraga, K. Shigemori, M. Koga, H. Nagatomo

On the Dynamic Detonation Parameters in Acetylene-OxygenMixtures with Varying Amount of Argon Dilution . . . . . . . . . . . . . . . . . . . 277B. Zhang, N. Mehrjoo, H.D. Ng, J.H.S. Lee

Contents Volume 1 XXVII

Strong and Weak Ignition in 2H2 + O2 behind Reflected Shocksin Two-Dimensional Navier-Stokes Simulations with DetailedChemistry . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 283A. Knisely, J.M. Austin, C. Bacon, A. Khokhlov

Velocity Fluctuations in the Interaction of Homogeneous, IsotropicTurbulence and a Detonation Wave . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 289S.M. Hussein, E.M. Blaiszik, E. Baydar, F.K. Lu

Deflagration-to-Detonation Transition of Methane-Oxygen Mixturesin Narrow Tubes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 295V.V. Golub, S.V. Golovastov, K.V. Ivanov, D.I. Baklanov, D.A. Lenkevich,A.L. Kotelnikov

Influence of Methane on Ignition Delays of Hydrogen at ImpulseDischarge from High Pressure Chamber . . . . . . . . . . . . . . . . . . . . . . . . . . . 301V.M. Bocharnikov, S.V. Golovastov, V.V. Golub

Experimental and Numerical Investigation of the HyShot II FlightExperiment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 307S.J. Laurence, S. Karl, K. Hannemann

On the Hypersonic Analogy for Problems of Detonation Inside 3DChannels . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 313V.A. Levin, I.S. Manuylovich, V.V. Markov

Point Measurement of Detonation Wave Speed . . . . . . . . . . . . . . . . . . . . . . 319F.K. Lu, N.K.M. Gupta, D.R. Wilson

Reflected Detonation Waves: Comparing Theory to Pressure and HeatFlux Measurements . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 325J. Damazo, J.E. Shepherd

Part V: Facilities

Experiments in a Combustion-Driven Shock Tube with an AreaChange . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 331B.E. Schmidt, B. Bobbitt, N.J. Parziale, J.E. Shepherd

Rapid Opening Valve Assisted by Magnetic Force for a DiaphragmlessShock Tube . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 337A. Abe, K. Sugahara, Y. Yamada

Improvement of a Diaphragmless Driver Section for a Small DiameterShock Tube . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 343S. Udagawa, Y. Hirose, W. Garen, T. Inage, M. Ota, K. Maeno

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Preliminary Experiment of the Drag Force Measurement by UsingStrain Gauge in the Hypersonic Flow . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 349Y. Hirose, S. Udagawa, R. Niwa, T. Inage, M. Ota, K. Maeno

A Numerical Investigation of the Flow through a New Fast ActingValve for Diaphragmless Shock Tubes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 355Manuel Gageik, Alexander Weiss, Igor Klioutchnikov, Herbert Olivier

Unsteady Drag Measurements for Hypersonic Shock Tunnel . . . . . . . . . . 361D.D. Joshi, F.K. Lu

Design and Commissioning of a New Lightweight Piston for the X3Expansion Tube . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 367D.E. Gildfind, R.G. Morgan, J. Sancho

High Mach Number Scramjet Test Flows in the X3 Expansion Tube . . . . 373D.E. Gildfind, J. Sancho, R.G. Morgan

Investigation of Nozzle Starting Problem and Its Applicationto Construct a Supersonic Wind Tunnel . . . . . . . . . . . . . . . . . . . . . . . . . . . . 379T. Yano, Kazuaki Hatanaka, Tsutomu Saito

Gasdynamics/Mechanical Hybrid Sabot Separation MethodRectangular-Bore Ballistic Range . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 385T. Imaizumi, A. Toyoda, Akihiro Sasoh

ISL Shock Tunnel Operation with ContouredMach-4.5-6-8-10-Nozzles for Hypersonic Test Applications . . . . . . . . . . . . 391B. Sauerwein, Robert Hruschka, P. Gnemmi, C. Rey, M. Bastide

Piezoelectric Pressure Microsensor Arrays for the SimultaneousMeasurement of Shock Wave Amplitude, Velocity and Directionat a Point . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 397G. Mirshekari, M. Brouillette, L. Fréchette

Reddy Tube Driven Table-Top Hypersonic Shock Tunnel . . . . . . . . . . . . . 403K.P.J. Reddy, R. Ramesh Babu, R. Murali, S. Saravanan

Spectral Characteristics of Pitot Noise . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 409H.G. Hornung, N.J. Parziale

Experimental Study of Moving Throat Plug in a Shock Tunnel . . . . . . . . 415J.K. Lee, C. Park, O.J. Kwon

Analysis of a Quick-Acting Diaphragmless Shock Tube Driver . . . . . . . . . 421R. Portaro, H. Nakayama, H.D. Ng

Contents Volume 1 XXIX

Part VI: Flow Visualization

Supersonic Flow over a Rectangular Open Cavity:Effect of Length-to-Depth Ratio . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 429V. Sridhar, S.L. Gai, H. Kleine

LIF Visualization of a Supersonic Deep-Cavity Flow . . . . . . . . . . . . . . . . . 435T. Handa, D. Ono

Application of the Polymer Based Pressure Sensitive Paint forQualitative and Quantitative Flow Visualisation in a Transonic Flow . . . 441K.H. Lo, H. Zare-Behtash, K. Kontis, N. Qin

Single-Plate-Imaging, Two-Wavelength Mach-ZehnderInterferometer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 447Naoki Hasegawa, Shigeru Yokota, Akihiro Sasoh

Background Oriented Schlieren Method Using Multi-scale PeriodicPattern . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 453Kazuaki Hatanaka, Tsutomu Saito

Orthogonal Projection Based Computationally Efficient Algorithmfor Deflection Tomography in High Speed Flow Studies . . . . . . . . . . . . . . . 459Biswajit Medhi, G.M. Hegde, K.P.J. Reddy, D. Roy, R.M. Vasu

NPLS Technique and Its Application on Complex Flow Field withShock Waves . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 465Shihe Yi, Yangzhu Zhu, Chen Zhi, Wu Yu

Toluene Laser-Induced Fluorescence (LIF) Imaging of SupersonicFlow within a Diverging Duct with Injectors in the SupersonicRegion . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 471K. Mohri, A. Wohler, B. Weigand, C. Schulz

Reconstruction of Unsteady and Axisymmetric Flow Field byColored-Grid Background Oriented Schlieren (CGBOS) Technique . . . . 477M. Ota, F. Leopold, F. Jagusinski, K. Maeno

Four-Dimensional LICT Density Measurement of UnsteadyShock-Vortex Flow Discharged from Two Inclined and CylindricalHoles Using High-Speed Camera . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 483Y. Miwa, T. Aratani, M. Ota, K. Maeno

Ultrafast Time Response Pressure-Sensitive Paint for UnsteadyShock-Wave Research . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 489Daiju Numata, Keisuke Asai

XXX Contents Volume 1

Quantitative Density Measurement of the Interaction Field of SideJet and Cross Flow by Colored-Grid Background Oriented Schlieren(CGBOS) Technique . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 495M. Ota, T. Inage, Y. Kikuma, H. Kawakami, Y. Miwa, K. Maeno

Investigation on Flow Structures of Supersonic Isolator Flow . . . . . . . . . . 501Chen Zhi, Shihe Yi, Wu Yu, Yangzhu Zhu

Visualization of Hypersonic Flat-Plate Boundary Layer in ShockTunnel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 507Qinghu Zhang, Shihe Yi, Chen Zhi, Yangzhu Zhu, Wu Yu

Part VII: Hypersonic Flow

Nonequilibrium and Rarefaction Effects in HypersonicMulticomponent Viscous Shock Layers . . . . . . . . . . . . . . . . . . . . . . . . . . . . 515V.V. Riabov

Hypersonic High-Enthalpy Flow in a Leading-Edge Separation . . . . . . . . 521N.R. Deepak, S.L. Gai, Sean O’Byrne, J.N. Moss

About the “Camel Effect” on Heat Transfer to a Sphere at HypersonicFlow Conditions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 527R. Adeli, P. Gnemmi, F. Seiler

Side Jet/Cross Flow Interaction at Hypersonic Re-entry Conditions . . . . 533R. Adeli, F. Seiler

Shock Standoff on Hemi-Spherical Bodies in Hypervelocity Flows . . . . . . 539F. Zander, P.A. Jacobs, R.J. Gollan, R.G. Morgan

Global Pressure- and Temperature- Measurements in 1.27-m JAXAHypersonic Wind Tunnel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 545Y. Yamada, T. Miyazaki, M. Nakagawa, S. Tsuda, H. Sakaue

Effects of Angle of Attack on the Behaviour of Imperfectionsin Thermal Protection Systems of Re-entry Vehicles . . . . . . . . . . . . . . . . . . 551R.C. Palharini, T.J. Scanlon, J.M. Reese

Hypersonic Interference Heating on Plates and Coneswith Three-Dimensional Protuberances . . . . . . . . . . . . . . . . . . . . . . . . . . . . 557C.S. Kumar, K.P.J. Reddy

Working towards Simulating Gas Giant Entry Radiationin an Expansion Tube . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 563C.M. James, D.E. Gildfind, R.G. Morgan, T.J. McIntyre

Contents Volume 1 XXXI

Numerical Predictions for Convective and Radiative Heatingof a Spacecraft Entering a Planetary Atmosphere . . . . . . . . . . . . . . . . . . . 569M.-C. Druguet, P. Boubert

Effect of the Shock Interaction on the Attitude Stability of theToroidal Ballute for Reentry Vehicle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 575H. Otsu, T. Abe

Effectiveness of Film Cooling over Large Angle Blunt Cones in HighSpeed Carbon Dioxide Flows . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 581S. Mohammed Ibrahim, R. Sriram, S. Chattopadhyay, G. Jagadeesh,K.P.J. Reddy

Tests of Hypersonic Inlet Oscillatory Flows in a Shock Tunnel . . . . . . . . . 587Zhufei Li, Wenzhi Gao, Hongliang Jiang, Jiming Yang

Emission Spectroscopy of a Mach Disk at Titan Atmospheric EntryConditions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 593Hadas Porat, Fabian Zander, Richard G. Morgan, Timothy J. McIntyre

New Mode of Instability and Double Mach Reflection in StationarySupersonic Gas Flow . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 599S. Gavrenkov, L. Gvozdeva

Edney IV Interaction Studies at Mach 5 . . . . . . . . . . . . . . . . . . . . . . . . . . . . 605A. Chettle, E. Erdem, K. Kontis

Diode-Laser-Based Driver Gas Detector for Hypersonic ShockTunnels . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 611Yedhu Krishna, Sean O’Byrne, Mark Aizengendler

Fluorescence Studies of Jet Mixing in a Hypersonic Flow . . . . . . . . . . . . . 617S. Brieschenk, R. Gehre, V. Wheatley, R.R. Boyce

Turbulent Spot Initiation Rates in Boundary Layersin a Shock Tunnel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 623D.J. Mee, G. Tanguy

Experimental Measurement of Aerodynamic Heat Transfer due toRadiative Transmission in High Enthalpy Flow around a Re-entryModel . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 629S. Srinath, K.P.J. Reddy

A Combined CFD/Characteristic Method for Prediction and Designof Hypersonic Inlet with Nose Bluntness . . . . . . . . . . . . . . . . . . . . . . . . . . . 635Wenzhi Gao, Zhufei Li, Jiming Yang

XXXII Contents Volume 1

Startability and Mach Reflection Hysteresis of Shortened BusemannIntakes for Axisymmetric Scramjet Engines . . . . . . . . . . . . . . . . . . . . . . . . 641H. Ogawa, S. Mölder, E.V. Timofeev, R.R. Boyce

The Direct Measurement of Base Drag for Hypersonic Vehicles . . . . . . . . 647Zhi-guo Lv, Guo-jun Li, Hua Jiang, Rong-juan Zhao, Gang Wang,Jun Huang

Measurements of Radiating Flow Fields in the Vacuum Ultraviolet . . . . . 653U.A. Sheikh, C. Jacobs, C.O. Laux, R.G. Morgan, T.J. McIntyre

Investigations about the Non-dimensional Heatflux Distributionfor Laminar Hypersonic Freestream . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 659Bibin John, Vinayak Kulkarni

Formation of Front Separation Zones during the Interaction of ShockLayer with Thin Temperature Wake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 665P. Georgievskiy, V.A. Levin, O. Sutyrin

Investigation of Hypersonic Boundary-Layer Transition UsingHigh-Speed Visualization Techniques . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 671S.J. Laurence, A. Wagner, K. Hannemann

N-Factor Correction of Free-Stream Noise at HighspeedBoundary-Layer Transition . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 677M. Thele, G. Schlöffel, F. Leopold, Ch. Mundt

Shock Tunnel Studies of the Hypersonic Flowfield around theHypervelocity Ballistic Models with Aerospikes . . . . . . . . . . . . . . . . . . . . . 681G. Balakalyani, S. Saravanan, G. Jagadeesh

Analysis of Thermochemical Nonequilibrium in Post-normal ShockFlow of Nitrogen . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 687Jae Gang Kim, Iain D. Boyd

Flowfield Establishment and Unsteadiness in Hypervelocity DoubleWedge Flows . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 693A.B. Swantek, A.M. Knisely, J.M. Austin

Experimental Studies on Unsteady Start/Unstart of High Speed AirIntakes with Moving Cowl . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 699P. Senthilkumar, T.M. Muruganandam

Experimental Studies on High Speed Air Intakes . . . . . . . . . . . . . . . . . . . . 705Amit Kumar Panigrahy, T.M. Muruganandam

Geometric Acoustics in High-Speed Boundary Layers . . . . . . . . . . . . . . . . 711N.J. Parziale, J.E. Shepherd, H.G. Hornung

Contents Volume 1 XXXIII

Numerical Predictions for the Hypervelocity Test Flow Conditionsof JF-16 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 717Z. Hu, Z. Jiang

Shock Tunnel Operation and Correlation of Boundary LayerTransition on a Cone in Hypervelocity Flow . . . . . . . . . . . . . . . . . . . . . . . . 723J.S. Jewell, J.E. Shepherd, I.A. Leyva

Effect of Sidewall Configurations on Hypersonic Intake Performance . . . 729Seihwan Kim, Ji Hyun Park, In-Seuck Jeung, Hyoung Jin Lee

The CARS Measurement of Nitrogen Vibrational and RotationalTemperatures around Wedge-Plate Model behind HypervelocityShock Wave . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 735D. Shirota, V.H. Bindu, M. Oguro, W. Eto, M. Ota, K. Maeno

Part VIII: Ignition

Experimental Study on Highly Diluted n-butylbenzene andn-butylbenzene/n-decane Mixtures behind Reflected Shock Waves . . . . . 743A. Comandini, T. Dubois, S. Abid, N. Chaumeix

Reflected-Shock Ignition of H2-O2-Ar Mixtures with Additionof H2S . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 749O. Mathieu, F. Deguillaume, E.L. Petersen

Part IX: Impact and Compaction

Dynamic Fracture Morphology of Bulk Metallic Glass Subjected toShock Compression . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 757Gauri Khanolkar, Shima Haghighat, Andrea M. Hodge,Katherine M. Flores, Veronica Eliasson

Evolution of Luminous Front at Impact of a 1 km/s Projectile intoSand Layer . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 763H. Yamamoto, Kazuyoshi Takayama, W. Cooper

Polymeric Flexible Syntactic Foam Composite for Shock Mitigation . . . . 769Jogi C. Gowda, Kunigal N. Shivakumar

Response of Polyurethane to Shock Waves: An ExperimentalInvestigation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 775V. Jayaram, Keshava Subba Rao, N. Thanganayaki, H.K.T. Kumara,K.P.J. Reddy

XXXIV Contents Volume 1

Part X: Industrial Applications

Using Shock Waves to Improve the Acoustic Properties of Closed-CellFoams . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 783M. Brouillette, C. Hébert, N. Atalla, O. Doutres

Dispersion and Size Reduction of Nanoparticles in Nanofluids UsingShock Waves . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 789H.K.T. Kumara, V. Jayaram, K.P.J. Reddy

Extinguishment of a Methane Air Diffusion Flame by Using BlastWave . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 795H. Torikai, S. Saito, A. Ito

Numerical Simulation of the Parametric Effect of a Tsunami WaveImpinging into a Coastal Forest for Damage Prevention . . . . . . . . . . . . . . 801S.M. Chang, G.S. Yeom, H. Youn

Author Index . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 807

Keyword Index . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 815