52nd 3AF International Conference

on Applied Aerodynamics Progress in Flow Control

Lyon, March 27-28-29, 2017

PROGRAMME

www.3af-aerodynamics2017.com

Buffet control on a swept wing © ONERA

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Thierry ALZIARY de ROQUEFORT ISAE-ENSMA (retired)Holger BABINSKY University of CambridgeAbderrahmane BAÏRI University of Paris WestEmmanuel BÉNARD ISAE-SUPAEROJean-Paul BONNET University of PoitiersJacques BORÉE ISAE-ENSMAPierre BRENNER Airbus Defence and Space Stéphane BURGUBURU Safran Aircraft EnginesYannick BURY ISAE-SUPAEROLaurent CAMBIER ONERASteeve CHAMPAGNEUX AirbusBruno CHANETZ ONERAPaola CINNELLA Arts et Métiers ParisTechJean COLLINET Airbus Defence and SpaceChristophe CORRE École Centrale de LyonMichel COSTES ONERAJean COUSTEIX ISAE Denis DARRACQ Airbus Jean DÉLERY 3AF and ONERAPhilippe DEVINANT University of OrléansPiotr DOERFFER Polish Academy of SciencesMichel DUMAS Safran Aircraft EnginesDenis GELY ONERANicolas GÉTIN MBDAPatrick GILLIÉRON RenaultPatrick GNEMMI ISLErwin R. GOWREE City University LondonFrancesco GRASSO IAT – CNAMVincent HERBERT PSA Peugeot CitroënYannick HOARAU University of StrasbourgDenis JEANDEL École Centrale de LyonEmilie JÉRÔME DGAAzeddine KOURTA University of OrléansViviana LAGO CNRSHadrien LAMBARÉ CNESOlivier ORLANDI Airbus Safran LaunchersDidier PAGAN MBDASandrine PALERM CNESPierre-Yves PAMART Safran Aircraft EnginesJean-Denis PARISSE University of Aix-MarseilleJoël RENEAUX ONERAJean-Pierre ROSENBLUM Dassault AviationWilliam S. SARIC Texas A&M UniversityFulvio SARTOR ONERAChristophe SICOT ISAE-ENSMAJean TENSI 3AF

www.3af-aerodynamics2017.com

52nd 3AF International Conference

on Applied Aerodynamics

Progress in Flow Control

Lyon, March 27-28-29, 2017 Automobile base flow control © PSA – Peugeot Citroën

52nd 3AF International Conference on Applied Aerodynamics Lyon, March 27-28-29, 2017

Progress in flow controlThe 3AF International Conference on Applied Aerodynamics is organized each year by the French Aeronautics and Space Society (3AF) in a different venue in France known for its activities in the field of aeronautics and/or space technology. The conference is an excellent opportunity for scientific exchanges within the aerospace community where aerodynamicists from industry, research institutions and academics meet. Scientists and engineers from other fields involving fluid mechanics are also welcome.

Each year the conference focuses on a different topic representative of current concerns in the field of aerodynamics. It is organized on the basis of five half-day technical presentations, each introduced by a keynote conference given by an expert in the field covered by the session. The conference is concluded by a technical visit in connection with the conference subject.

In 2017, the conference will be hosted by the École Centrale de Lyon.

The 52nd 3AF International Conference on Applied Aerodynamics will focus on recent research in flow-control techniques aiming at the development of greener vehicles, more comfortable means of transportation, environmental “friendliness” and sustainability. This involves improvements in aerodynamics performance, reduction of fuel consumption and emissions, as well as reduction of other negative impacts on the environment such as noise, wake vortices, soiling, etc. The techniques involved are passive and active devices, contouring, energy deposition, morphing, but not limited to the aforementioned.

Flow control is present in a large number of applications including aircraft and UAVs, helicopters, automobiles, trains, ships, wind turbines, missiles, space launchers, turbo-machinery, environmental management in buildings, combustion chambers, etc.

The experimental, theoretical and numerical aspects dealing with fundamental and applied research as well as industrial application will be considered.

CONFERENCE LOCATION: ORGANIZATION:

ECOLE CENTRALE DE LYON 36 avenue Guy de Collongue 69134 ÉCULLY (France)

MONDAY 27 MARCH 2017

08:00 Registration & Welcome Coffee

09:00 Conference Welcome

10:00 Keynote Conference n°1: P. SCHMIDT – Imperial College London

10:45 Session n°1a: Control theory and applications / Session n°1b: High speed and internal flows

14:15 Keynote Conference n°2: C. BAILLY – École Centrale de Lyon

15:00 Session n°2a: Acoustics / Session n°2b: Rotating bodies

19:00 Welcome Cocktail

TUESDAY 28 MARCH 2017

09:00 Keynote Conference n°3: C. LAUX – École Centrale de Paris

09:45 Session n°3a: Transition control / Session n°3b: Wake control / Session n°3c: Other flow investigations

14:15 Keynote Conference n°4: M. X. MEYER - Airbus

15:00 Session n°4a: Wing separation control / Session n°4b: Ground vehicles

20:00 Award of the 3AF International Conference on Applied Aerodynamics and Banquet

WEDNESDAY 29 MARCH 2017

09:00 Keynote Conference n°5: A. SEIFERT – Tel Aviv University

09:45 Session n°5a: Actuators and sensors. Skin friction control / Session n°5b: Closed loop control. Morphing

14:30 Technical Visit

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Circulation control of the flow past a wing © Technische Universität Braunschweig

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08:00 REGISTRATION

09:00 CONFERENCE WELCOME Christian MARI (Chairman of the High Scientific Council, 3AF) Frank DEBOUCK (Director, École Centrale de Lyon)

09:30 KEYNOTE CONFERENCE N°1: Linear control of oscillator and amplifier flows Peter SCHMID (Imperial College London)

ROOM 1 ROOM 2

Session n° 1a: Control theory and applications Chairperson: Laurent JACQUIN (ONERA)

Session 1b: High speed and internal flows Chairperson: Jacques BORÉE (ISAE-ENSMA)

10:15 Non-linear model reduction: a comparison between POD-Galerkin and POD-DEIM methods D. Sipp, M. Fosas and P. Schmid (ONERA/Imperial College London)

Plasma actuator for supersonic flow control around a flat plate S. Hamdoun, B. Liani and J.-D. Parisse (University Abou Bekr Belkaïd/French Air Force Academy)

10:45 Reinforcement learning strategies for closed-loop control in fluid dynamics C. Pivot, L. Mathelin, L. Cordier, F. Guéniat, and B. Noack (Pprime Institute/ISAE-ENSMA/Florida State University)

Suppression of laminar SWBLI separation by spark discharge at low supersonic Mach number P. A. Polivanov, A. A. Sidorenko and A. A. Maslov (Khristianovich Institute of Theoretical and Applied Mechanics)

11:15 COFFEE BREAK

11:45 Integral equations for boundary layers with vortex generators G. de Oliveira, N. Timmer and B. W. van Oudheusden (Delft University of Technology)

Tomographic-PIV investigation of the 3D separation behavior of a micro-ramp controlled SWBLI S. Nayak K, R. H. M. Giepman, F. F. J. Schrijer and B. W. van Oudheusden (Delft University of Technology)

12:15 On the free flight behavior of a spinning projectile fitted with fins: a comparative study between twisted fins versus canted ones C. Decrocq, B. Martinez, P. Gnemmi, M. Albisser and S. Dobre (French-German Research Institute of Saint-Louis)

Impact of large scale surface roughness on aero-engines at incidence C. Coles, A. Coschignano, H. Babinsky, C. Sheaf and E. Platt (University of Cambridge/Rolls Royce PLC)

12:45 Large-Eddy Simulation of rod-airfoil flow configuration in the subcritical turbulent regime by using the lattice Boltzmann method H. Touil, B. Bazin, J.-C. Giret, S. Malik, E. Lévêque, J. Boudet, D. Ricot and A. Sengissen (Communication & Systèmes/LMFA/Renault/Airbus)

Flow control in duct flows E. Garnier, J.-C. Boniface and P. Grenson (ONERA)

13:15 LUNCH

L’école autour de son stade: ©ECL-J.Hamoy

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14:15 KEYNOTE CONFERENCE N°2: An experimental investigation of wall pressure fluctuations caused by a turbulent boundary layer Christophe BAILLY (École Centrale de Lyon)

ROOM 1 ROOM 2

Session n° 2a: Acoustics Chairperson: Daniel JUVÉ (LMFA-École Centrale de Lyon)

Session n° 2b: Rotating bodies Chairperson: Isabelle TRÉBINJAC (LMFA-École Centrale de Lyon)

15:00 Measurement of density fluctuations in free jets by a Rayleigh scattering based method B. Mercier, E. Jondeau, T. Castelain and C. Bailly (LMFA-École Centrale de Lyon)

Intercomparison of the effects of different free-stream disturbances on compressible transitional boundary layers in a low-pressure turbine cascade K. Matsuura, K. Matsui and N. Tani (Graduate School of Science and Engineering, Ehime University-IHI Corporation)

15:30 Intermittency and nonlinearities in the near-field of a temporal round jet at Mach 2 P. Pineau and C. Bogey (LMFA-École Centrale de Lyon)

Passive flow control application for rotorcraft in transonic conditions F. Tejero, P. Doerffer, P. Flaszynski and O. Szulc(Institute of Fluid-Flow Machinery-Polish Academy of Sciences)

16:00 Controlling unsteady cavity flows using internal structures K. Knowles, D. Bacci, A. J. Saddington, B. Newby and N. J. Taylor (Cranfield University)

Streamwise vortex generator for separation reduction on wind turbine rotor J. Martinez Suarez, P. Flaszynski and P. Doerffer (Institute of Fluid-Flow Machinery-Polish Academy of Sciences)

16:30 COFFEE BREAK

17:00 Fluid structure interactions and launcher design J. Collinet (Airbus Safran Launchers)

Plasma and fluidic jet actuators for circulation control around wind turbine airfoils A. Leroy, C. Braud, V. Jaunet, S. Baleriola, E. Guilmineau, S. Loyer, P. Devinant and S. Aubrun (Prisme Institute/École Centrale de Nantes)

17:30 Columnar vortex generator for flow control over a ski-jump ramp R. Bardera-Mora, M. León-Calero and J. Nova-Trigueros(Instituto Nacional de Técnica Aeroespacial (INTA) Technical University of Madrid)

19:00 COCKTAIL

Reduction of the noise due to a CROR/pylon interaction © ISAE - Supaero Control of a bow shock wave by a plasma discharge © ONERA

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9:00 KEYNOTE CONFERENCE N°3: Plasma assisted combustion: fundamentals and applications to flame stabilization Christophe LAUX (École Centrale de Paris)

ROOM 1 ROOM 2 ROOM 3

Session n°3a: Transition control Chairperson: Chris ATKIN (City, University of London)

Session 3b: Wake control Chairperson: Elisabeth FOURNIER (BMW)

Session 3c: Other flow investigations Chairperson: Kevin KNOWLES (Cranfield University)

09:45 Real-time feedback control of TS waves H. Vemuri, R. Bosworth, J. F. Morrison and E. Kerrigan (Imperial College London)

Synchronization control of a Von Kàrmàn vortex street using a DBD actuatorV. Parezanovic, Y. Bury and L. Joly (ISAE-SUPAERO)

Numerical simulation of runback ice forming downstream from a thermal ice protection system K. Szilder (National Research Council of Canada)

10:15 Effect of surface vibration on the excitation and evolution of Tollmien-Schlichting wavesE. Gowree and C. J. Atkin (City, University of London)

Study of flow control for a D-shaped vehicle model E. Guilmineau and G. Bhati (École Centrale de Nantes)

Reynolds and Mach number effects in rectangular duct flowD. Modesti, S. Pirozzoli and F. Grasso (Sapienza Università di Roma/CNAM - DynFluid Laboratory)

10:45 Control of Transonic Buffet Through Deployable FlapsS. Pirozzoli and A. Memmolo (Sapienza Università di Roma)

Influence of the pitch on the wake modes of the squareback Ahmed body G. Bonnavion, O. Cadot, V. Herbert, S. Parpais, R. Vigneron and J. Délery (PSA Peugeot Citroën/Renault/ GIE S2A)

Open-source CFD code assessment for lighter-than-air aerodynamic flows simulations G. Joubert (A-NSE)

11:15 COFFEE BREAK

11:45 Linear and nonlinear wall forcing of the secondary crossflow instabilityE. van Bokhorst and C. Atkins (City, University of London)

Reactive control of large-scale structures in a turbulent wakeE. Varon, Y. Eulalie, S. Edwige, P. Gilotte and J.-L. Aider (ESPCI/Université Pierre et Marie Curie/Plastic Omnium)

Discrete vortex method for a detached flow on a two-airfoil configuration at high angle of attack T. Faure, V. Drouet and O. Montagnier (French Air Force Academy)

12:15 Experimental investigation of the vorticity amplification on a swept wing with a blunt leading edgeI. Fumarola, M. Gaster and C. Atkin(City, University of London)

Numerical and experimental analysis of rotating wheel in contact with the groundM. Kulak, M. Karczewski, P. Lesniewicz, K. Olasek, B. Hoogterp, G. Spolaore and K. Jòzwik (Lodz University of Technology/Saxion Enschede/ PSA Peugeot Citroën)

Synthetic jet effect on theaerodynamic performances of NACA 0015 airfoilK. Boualem, A. Azzi and T. Yahiaoui(Sciences and Technology Universityof Oran)

12:45 Attachment line transition control using passive and active devicesM. Forte, G. Casalis, O. Vermeersch, C. François and E. Piot (ONERA)

13:15 LUNCH

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14:15 KEYNOTE CONFERENCE N°4: Towards the industrial application of active flow control in aerospace Michael X. MEYER (Airbus)

ROOM 1 ROOM 2

Session n°4a: Wing separation control Chairperson: Joël RENEAUX (ONERA)

Session n°4b: Ground vehicles Chairman: Damien CHACATON (Volvo GTT)

15:00 DES prediction of a 3-element high-lift airfoil with a blown flapBo Ouyang, Y. Yao and A. Bouferrouk (University of the West of England)

An experimental study on truck rear side-skirt and bumper flow I. Vallina-Garcia, R.G. Stephens and H. Babinsky (University of Cambridge)

15:30 Numerical sizing of active flow control concepts on the outer wingJ.-P. Rosenblum, P. Vrchota, S. Wallin, P. Eliasson, P. Iannelli, V. Ciobaca, J. Wild, J.-L. Hantrais-Gervois and M. Costes (Dassault Aviation/VZLU/FOI/CIRA/DLR/ONERA)

Experimental study of the wake of a simplified truck model in ground proximity in view of defining a control strategy for drag reductionM. Szmigiel, M. Michard, T. Castelain, D. Juvé and D. Chacaton (Volvo Group Truck/LMFA-École Centrale de Lyon)

16:00 On the use of fluidic oscillators to trim and control a swept-back wing & a tailless aircraft modelP. Tewes, M. Jentzsch, L. Taubert and I. Wygnanski (The University of Arizona/Tel-Aviv University)

Adaptive boat-tail under variable cross-windJ. M. Garcia de la Cruz, R. D. Brackston, G. Rigas and J. F. Morrison (Imperial College London)

16:30 COFFEE BREAK

17:00 Flow control at trailing edge of wings and profiles: an overview of the AFLoNext projectF. Sartor, M. Minervino, J. Wild, S. Wallin, H. Maseland, J. Dandois, V. Soudakov and P. Vrchota (ONERA/CIRA/DLR/KTH/TsAGI/VZLU)

Drag reduction for the flow past a 47° Ahmed bodyS. Edwige, Y. Eulalie, P. Gilotte and I. Mortazavi (Plastic Omnium/CNAM Paris)

17:30 Influence of vane vortex generators on transonic wing buffet: further analysis of the BUCOLIC experimental datasetL. Masini, S. Timme, A. Ciarella and A. Peace (University of Liverpool/Aircraft Research Association)

Wake modes control of a real minivan for drag reductionG. Bonnavion, O. Cadot, V. Herbert, S. Parpais, R. Vigneron and J. Délery (ENSTA-ParisTech/PSA Peugeot Citroën/GIE S2A)

18:00 Nonlinear system identification of NACA 0015 high lift system under dual location active flow controlB. Alstrom, S. Moreau, N. Atalla, E. Bolt and P. Marzocca (University of Sherbrooke/Clarkson University/RMIT University)

Instantaneous and time averaged pressure analysis at the rear of a SUV vehicle for active flow control optimizationY. Eulalie, P. Gilotte, E. Fournier, T. Schutz, S. Johnson, D. Holst, D. Wieser and C. N. Nayeri (Plastic Omnium/BMW Group/Technische Universität Berlin)

20:00 AWARDS & BANQUET

Base flow control © Pprime InstituteVG’s in transonic flow © ONERA

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09:00 KEYNOTE CONFERENCE N° 5: The use of steady suction and pulsed blowing for efficient boundary layer separation control Avraham SEIFERT (Tel Aviv University)

ROOM 1 ROOM 2

Session n°5a: Actuators and sensors. Skin friction control Chairperson: Philippe PERNOD (IEMN - École Centrale de Lille)

Session n°5b: Closed loop control. Morphing Chairperson: Jonathan MORRISON (Imperial College London)

09:45 Development of simplified boundary condition of SaOB actuator based on high-fidelity CFD simulations P. Vrchota, A. Prachař, P. Hospodá, D. Dolgopyatand A. Seifert (VZLU/Tel Aviv University)

Machine learning control of the turbulent wake past a 3D bluff body R. Li, B. R. Noack, L. Cordier, J. Borée andF. Harambat (Pprime Institute/LIMSI/TechnischeUniversität Braunschweig/PSA Peugeot-Citroën)

10:15 MEMS calorimetric shear stress sensor for flow control applications J. Weiss, E. Jondeau and A. Giani (École de technologiesupérieure-Montréal/École Centrale de Lyon/Universityof Montpellier)

Drag reduction of a bluff body by feedback control of bistability R. D. Brackston, J. M. Garcia de la Cruz, A. Wynn,G. Rigas and J. F. Morrison (Imperial College London)

10:45 Wall shear stress and flow direction micro-sensor for separation detection and flow control C. Ghouila Houri, R. Sindjui, Q. Gallas, E. Garnier,A. Merlen, R. Viard, A. Talbi and P. Pernod(IEMN-École Centrale de Lille/ONERA)

Bi-modality in the wakes of simplified road vehicles: simulation and feedback control A. Morgans, L. Dalla Longa and O. Evstafyeva(Imperial College London)

11:15 COFFEE BREAK

11:45 Control of boundary-layer streaks induced by freestream turbulence using plasma actuators K. Gouder, A. M. Naguib, P. Lavoie and J. F. Morrison(Imperial College London/Michigan State University)

12:15 Staggered three-dimensional cavities as a possible method for skin friction drag reduction.E. Gowree and C. J. Atkin (City, University of London)

12:45 Electroactive morphing of a supercritical wing for increasing the aerodynamic performanceG. Jodin, N. Simiriotis, V. Temtching, D. Szubert,Y. Hoarau, J. Scheller, J. F. Rouchon and M. Braza(IMFT/Laplace Institute/ICUBE)

Unsteady parametrization of a morphing wing design for improved aerodynamic performance C. Abdessemed, Yufeng Yao, A. Bouferrouk andP. Narayan (University of the West of England)

Further insight into the mechanism of stall delay on an aerofoil with an undulating leading edgeE. Talboys, C. Jagadeesh, E. Gowree and A. Pinelli(City, University of London)

13:15 LUNCH14:30

TECHNICAL VISIT17:00

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Technical visits scheduled on Wednesday, March 29, 2017

The technical visits proposed in the framework of the AERO2017 Conference to the pre-registered participants will give them the opportunity to discover the following facilities of the Fluid Mechanics and Acoustics Laboratory (LMFA) on the campus of École Centrale de Lyon:

• Atmospheric boundary layer wind tunnel. This wind tunnel, 14m long, 3.7m large and 2m high, allows to study dispersion in the atmospheric boundary layer for flow speeds from 1 to 8 m/s. Taking pictures of the model present in the wind tunnel at the time of the visit is strictly prohibited.

• Anechoic wind tunnels. These facilities combine open-circuit wind tunnels and an anechoic chamber of large size (volume of the plenum: 720 m3). They allow the experimental study of the aeroacoustic properties of wall-bounded flows (fan noise, airframe noise) or free flows (jet noise) as well as the development of measurement techniques for aeroacoustics.

• CREATE (Compresseur de Recherche pour l’Étude des effets Aérodynamiques et TEchnologiques / Research Compressor for the Study of Aerodynamic and Technological Effects) test rig. This large-scale test instrument, a three-stage research compressor specially designed for the validation of CFD tools, allows to perform both aerodynamic and mechanical parametric studies.

All facilities proposed for the technical visits are located in a Restricted Access Zone. Conference participants willing to take part in these visits must therefore be pre-registered and also provide an identity document prior to the visits. This ID will be used to deliver the access clearance. For the visits to take place in the best possible material conditions, the total number of participants is limited to about 30 persons (divided into 3 groups).

Planning of the visits

Start End Group #1 Group #2 Group #3

2.30 pm 3.10 pmAtmospheric boundary layer

wind tunnel (H10)Anechoic wind tunnels (KCA) CREATE Test rig (I11)

3.15 pm 3.55 pm CREATE Test rig (I11)Atmospheric boundary layer

wind tunnel (H10)Anechoic wind tunnels (KCA)

4.00 pm 4.40 pm Anechoic wind tunnels (KCA) CREATE Test rig (I11)Atmospheric boundary layer

wind tunnel (H10)

The conference will take place in the École Centrale de Lyon.

Getting to Conference location

École Centrale de Lyon 36 avenue Guy de Collongue 69134 ÉCULLY (France)

Bus: Line 55 Stop: “Campus Lyon Ouest”

More information: http://www.tcl.fr/en

Conference Shuttle

A dedicated shuttle is organized from Lyon Center (30, Cours de Verdun) to École Centrale in order to access on time to the Conference. The detailed schedule is available onlinewww.3af-aerodynamics2017.com and at the Welcome Desk.

©ECL-J.Hamoy

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École Centrale de Lyon - 36, avenue Guy de Collongue - 69134 ÉCULLY (France)

LANGUAGE

Official language for the conference is English.

REGISTRATION

Delegates including Chairpersons and Speakers are requested to register and settle registration fees prior the conference. Access to technical visit is controlled for security reasons.

Registration fees include: Conference session attendance, Conference documentation, coffee breaks, lunches, banquet on Tuesday, March 28, 2017, access to the technical visit and Conference proceedings.

All prices quoted are in EURO. Registration fees not subject to VAT.

3AF Individual Member € 650.00 Speaker/Chairpersons € 650.00 Participant € 900.00 Academics/Student/PhD € 400.00 Additional conference banquet ticket for accompanying person € 60.00

REGISTRATION FORM AND PAYMENT

On line registration on: http://3af-aerodynamics2017.evenium.net

Complete online form and follow payment indication. Upon receipt of your payment an invoice and a recipe will be sent. These are to be shown at the Conference Welcome Desk.

CANCELLATION POLICY

At less than 7 days from the conference, a € 350 cancellation fee will apply to participants, speakers and chairpersons, € 250 to Academics and students / PhD.

Delegates who do not cancel before the start of the conference will be liable to the full registration fee.

PUBLICATION

Authors of the best papers will be invited current April to propose an extension of their works for publication in a special issue of the International Journal of Numerical Methods for Heat & Fluid Flow* dedicated to the conference. These extended versions must be original, written according to the journal’s standards and submitted online** before May 31, 2017. Each paper is reviewed by the guest-editor and, if it is judged suitable for publication, is sent to at least two independent referees for double blind peer review.

*IJNMHFF,Impact Factor: 1.399, 2014; Journal Citation Reports®, Thomson Reuters, 2015) http://emeraldgrouppublishing.com/products/journals/journals.htm?id=hff - **http://mc.manuscriptcentral.com/hff#sthash.w1PkH6Vd.dpuf

SECRETARIAT

For more information please contact:

3AF Executive Secretariat - 6, Rue Galilée – 75016 Paris, France - Fax: +33 (0)1 56 64 12 31 Anne Venables - E-mail: secr.exec@aaaf.asso.fr – Phone: +33 (0)1 56 64 12 30 Aude Lurbe - E-mail: aude.lurbe@aaaf.asso.fr – Phone: +33 (0)1 56 64 12 37

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MERCURE LYON CENTRE CHATEAU PERRACHE ****

12, Cours de Verdun Rambaud 69002 LYON Tel: (+33) 4.72.77.15.00 Web: http://www.mercure.com/fr/hotel-1292-hotel-mercure-lyon-centre-chateau-perrache/index.shtml

KYRIAD LYON CENTRE PERRACHE

26, cours de Verdun Perrache 69002 LYON Tel: (+33) 4.78.71.17.47 Web: www.kyriad.com/en/hotels/kyriad-lyon-centre-perrache

IBIS LYON CENTRE PERRACHE ***

28, Cours de Verdun Perrache 69002 LYON Tel: (+33) 4.78.37.56.55 Web: http://www.accorhotels.com/en/hotel-2751-ibis-lyon-centre-perrache/index.shtml

Please contact the Executive Secretary for information: Anne Venables - 6, rue Galilée - 75016 Paris, France Tél +33 (0)1 56 64 12 30 - secr.exec@aaaf.asso.fr

Make your reservation as soon as possible.

We recommend hotels in the center of Lyon. Dedicated shuttle is available near to these three hotels. Special rates are negotiated with the following hotels:

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ONERA, First Aerospace Research Player in France.

ONERA (Office National d’Etudes et Recherches Aérospatiales) is the French Aerospace Research Center.

It is a public research establishment, with both industrial and commercial responsibilities, reporting to the French Ministry of Defense and enjoying financial independence. With 2,000 employees, including 1,500 scientists, engineers and technicians, the expertise of ONERA covers all the scientific disciplines involved in aircraft, spacecraft, turbomachinery and missile design. It makes ONERA an essential partner in the French and European aeronautics and space community.

Its main missions are:

• to assist government agencies in charge of coordinating civil and military aerospace policy,

• to direct and carry out aerospace research,

• to design, produce and operate the resources needed

• to perform research and testing for manufacturers,

• to make available and commercialize the results of its research and facilitate application of this research by industry, including non-aerospace sectors,

• to support the French training policy for scientists and engineers.

Since its creation in 1946, ONERA has worked on all the major French and European aeronautical and space programs, including Mirage, Concorde, Airbus, Ariane, Rafale, etc… It’s continuously upgrading its research and test facilities, some of them exhibiting unique capabilities.

The Royal Aeronautical Society is “the one multidisciplinary professional institution dedicated to the global aerospace community”. The RAeS is the world’s only professional body which caters for the entire aerospace

community. Throughout the world’s aerospace community the name of The Royal Aeronautical Society is both well-known and well respected.

The Royal Aeronautical Society has a range of Specialist Interest Groups, covering all aspects of the aerospace world, serving the interests of enthusiasts and industry professionals alike.

Through their conferences and lectures, the Groups consider significant developments in their field, stimulate debate and facilitate action on key industry issues, reflecting the constant innovation and progress in aviation. In addition, the Groups, acting as focal points for all enquiries, form a vital interface between the Society and the world at large.

The activities of the Aerodynamics Group cover a wide range of topics of interest to industry, research establishments and universities. Several members of the group have been active in the creation of the TSB funded UK Aerodynamics Centre. The wind tunnel facility review initiated by the Group has been taken up by the Aero Centre. The Group is trying to work more closely with the AAAF and the AIAA Applied Aerodynamics Technical Committee. The Group organizes a regular Applied Aerodynamics Conference as well as hosting the Lanchester Named Lecture.

Strengthened by 150 years of experience, the mission of École Centrale de Lyon is to educate its students to become generalist

engineers and multi-disciplined post-graduate leaders in their field.

With 6 research units located on campus, all of which are part of the CNRS, or the French National Centre for Scientific Research, the School intrinsically combines Academic Education and Research, equipping you with the skills you need to progress towards your ideal career path.

Well-established as a key institution within its field, conscious of globalisation and of the increased competition that comes with it, for forty-five years the School has formed agreements with universities from all of the world that pertain to the awarding of double degrees and other forms of partnership.

The School also maintains permanent contact with leading industrial groups, regularly present on campus, who also provide you with opportunities to take part in periods of immersion within the workforce, allowing you to accumulate up to 18 months of professional experience.

Over and above the scientific and technical skills that the School undeniably imparts to its students, École Centrale de Lyon provides you with an open-minded, wide-ranging vision of the world as well as an approach towards the humanities and social sciences that grant our graduates the Centrale Lyon advantage.

Our purpose is to ignite and celebrate aerospace ingenuity and collaboration, and its importance to our way of life.

Our promise is to be your vital lifelong link to the aerospace community and a champion for its achievements.

One Remarkable Fact Says It All: Since 1963, members from a single professional society have achieved virtually every milestone in modern American flight. That society is the American Institute of Aeronautics and Astronautics. With more than 35,000 individual members and 100 corporate members, AIAA is the world’s largest technical society dedicated to the global aerospace profession. Created in 1963 by the merger of the two great aerospace societies of the day, the American Rocket Society (founded in 1930 as the American Interplanetary Society), and the Institute of the Aerospace Sciences (established in 1933 as the Institute of the Aeronautical Sciences), AIAA carries forth a proud tradition of more than 80 years of aerospace leadership.

This is the place for everything, from exploring our history and purpose … to catching up on the latest news … Make sure you check out our prestigious Honors & Awards programs.

Recognizing excellence is one the most important contributions we make. Serving this elite audience and its historic mission is our commitment and our privilege. Now we invite you to learn more about AIAA – and share in the vision and excitement of this inspiring industry.

The Council of European Aerospace Societies was formed in 1993 as the Confederation of European Aerospace Societies in recognition of the increasingly international nature of the aerospace business. The transition from Confederation to Council took place in 2003 with the intention of providing improved collaboration, legal status and use of the resources

of the constituent Societies.

In the mid 1980s Europe’s main professional aerospace societies, after having had bilateral exchanges for a long time, recognized the increasingly international nature of aerospace business and the strength of European industrial alliances by beginning to develop close working relationships.

This culminated in the formation of the Confederation of European Aerospace Societies (CEAS) during the 1992 Farnborough Airshow and the official signing of the CEAS Constitution at the 1993 Paris Airshow.

Later on, in 2003, the Constituent Societies realized that a deeper collaboration was necessary which would provide CEAS with a legal status and more flexible resources. The new status transformed in 2006 the former Confederation into a Council and gave CEAS legal support under the Belgian law.

Apart from the consideration of CEAS as an association of national Societies, two branches have been established: one for aeronautics and one for space chaired by relevant professionals. These branches will be composed by technical committees with individual members and will be coordinated by a director who will manage the activities.

Today CEAS comprises fifteen member societies with a combined roughly 35.000 individual members.

The Aerodynamic Research Group of TE Connectivity manufactures pressure and temperature scanning systems. Primarily used for Windtunnel, Flight Test and Turbomachinery Testing, the scanning systems provide high accuracy measurement solutions for multi-channel test installations. Windtunnel and Flight

Testing use ESP pressure scanners for their compact size and high accuracy. Complete windtunnel system solutions are accomplished with the DTC Initium, 8400 System or through 3rd party data systems. Turbomachinery Testing use the NetScanner™ System Models like 9116, 9146 to for pressure and temperature scanning on or near the gas turbine or the 98RK-1 rack mount pressure scanning system with 9816 scanners for control room installations.

52nd 3AF International Conference on Applied Aerodynamics Lyon, March 27-28-29, 2017

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