international conference on applied aerodynamics ... of the 3af international conference on applied...

50thedition of the 3AFInternational Conference on Applied AerodynamicsForthcoming Challenges for AerodynamicsToulouse, France – March 30, 31, April 1, 2015

« Convertible configuration. Computation - © Onera »

http://3af-aerodynamics2015.com

PROGRAMME

50thedition of the 3AFInternational Conference on Applied AerodynamicsForthcoming Challenges for Aerodynamics

Toulouse, FranceMarch 30, 31, April 1, 2015

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50th edition of the 3AF International Conference on Applied Aerodynamics, Toulouse, March 30, 31, April 1, 2015

Holger BABINSKY University of CambridgeAbderrahmane BAÏRI University of Paris WestEmmanuel BÉNARD ISAE Jean-Paul BONNET University of PoitiersJacques BORÉE ISAE - ENSMAPierre BRENNER Airbus Defence and Space Stéphane BURGUBURU Safran SnecmaYannick BURY ISAE Laurent CAMBIER OneraBruno CHANETZ OneraPaola CINNELLA Arts et Métiers ParisTechJean COLLINET Airbus Defence and SpaceMichel COSTES OneraJean COUSTEIX ISAE Denis DARRACQ Airbus Jean DÉLERY 3AF and OneraPhilippe DEVINANT University of OrléansPiotr DOERFFER Polish Academy of SciencesMichel DUMAS Safran SnecmaAnne GAZAIX Airbus Nicolas GÉTIN MBDAPatrick GILLIÉRON RenaultPatrick GNEMMI ISLFrancesco GRASSO IAT - CNAMVincent HERBERT PSA Peugeot CitroënDenis JEANDEL Ecole Centrale de LyonEmilie JÉRÔME DGAAzeddine KOURTA University of OrléansViviana LAGO CNRSHadrien LAMBARÉ CNESOlivier ORLANDI Safran HeraklesDidier PAGAN MBDASandrine PALERM CNESPierre-Yves PAMART Safran SnecmaJean-Denis PARISSE University of Aix-MarseilleJoël RENEAUX OneraJean-Pierre ROSENBLUM Dassault AviationWilliam S. SARIC Texas A&M UniversityJean TENSI 3AF

www.3af-aerodynamics2015.com

High-speed flow control - © ISL

CONFERENCE LOCATION: ORGANIZATION:

ISAE, Campus SUPAEROComplexe Scientifique de RANGUEIL10 avenue Edouard Belin31400 Toulouse, France


Forthcoming Challenges for AerodynamicsThe 50th 3AF Conference on Applied Aerodynamics will be an occasion to focus on forthcoming challenges for aerodynamics arising from the ever growing demands for “greener vehicles”, more comfortable means of transportation, alternative energy sources and environmental “friendliness”. This involves improvements to fuel consumption and pollutant emissions, as well as reduction of negative impacts on the environment such as noise, wake vortices, soiling, etc. There is also a pressure to increase efficiency and reliability of wind-turbines, etc. Green or sustainable building construction requires careful consideration of ventilation systems

with reduced energy cost. There is also a constant need for better performance increased range and improved stealth for military aircraft and missiles.

Aerodynamics plays an important and often key role in all these domains so that such performance improvement can only be reached through decisive progress and even breakthrough in the many domains of aerodynamics including: flow modelling and physical understanding of complex phenomena, predictive and design methods, experimental investigation and data interpretation, etc.

All domains of application of aerodynamics will be of interest: aircraft and UAV, engines, missiles and space launchers, airships, terrestrial vehicles, buildings, wind-turbine farms, ships, trains, Flow simulation past an automobile © Onera

MONDAY 30 MARCH 2015

08:00 Registration09:00 Conference Welcome09:30 Keynote Conference N°110:15 Session n°1: Challenges in flow modelling and numerical simulation14:15 Keynote Conference N°215:00 Session n°2: Experimental Challenges

TUESDAY 31 MARCH 2015

08:30 Keynote Conference N°309:15 Session n°3: New technologies14:00 Keynote Conference N°414:45 Session n°4: New configurations18:30 The 2015 Lanchester Lecture, organized by the Royal Aeronautical Society20:00 Award of the 3AF International Conference on Applied Aerodynamics and Banquet

WEDNESDAY 1 APRIL 2015

08:45 Keynote Conference N°509:30 Session n°5: Multiphysics and optimization14:30 Technical visit: Airbus17:00 End of conference

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5 09:00 CONFERENCE WELCOMEMichel Scheller (President, French Aeronautics and Astronautics Society)Olivier Lesbre (Director, Institut Supérieur de l’Aéronautique et de l’Espace)

09:30 KEYNOTE CONFERENCE N°1: Turbulence prediction in aeronautics and neighboring fieldsPhilippe Spalart (Boeing Company)

Session n° 1: Challenges in flow modelling and numerical simulation

Session n° 1a: Flow separationChairperson: Jean-François Boussuge (CERFACS)

Session n° 1b: Complex flowsChairperson: Alain Merlen(Onera)

Session n° 1c: MethodologiesChairperson: Jean-MarieLe Gouez (Onera)

10:15 Application of a hybrid variational multiscale model to massively separated flowsE. Itam, S. Wornom, B. Koobus and A. Dervieux (University of Montpellier / LEMMA / INRIA-Sophia Antipolis)

Body force modeling for efficient analysis of intake-fan interactionsE. William, W. Thollet, F. Blanc,G. Dufour and X. Carbonneau (Airbus Operations SAS/ISAE-Supaero)

A Contribution to the wayof the all-Mach numberN. Chauchat, E. Schall, N. Lantos and G. Leroy (UFR Sciences et Techniques de Pau / Onera / SAFRAN - Turbomeca)

10:45 Incompressible flow simulations around a diamond wingE. Guilmineau, M. Visonneau andS. Toxopeus (LHEEA-Ecole Centrale de Nantes / MARIN-Wageningen)

Parallel anisotropic 3D mesh adaptation for unsteady turbulent flowsE. Hachem, L. Billon, J. Sari,F. Cauneau and Y. Mesri(MINES - ParisTech)

Instabilities in helical vortex systems: linear analysis and nonlinear dynamicsC. Selçuk, I. Delbendeand M. Rossi (LIMSI-CNRS /University Pierre et Marie Curie)

11:15 COFFEE BREAK

11:45 Mach number effect on buffeting flow in a half wing/body configurationF. Sartor and S. Timme(University of Liverpool)

Study of a cooling deviceof confined impacting air jets on a heating cylinderN. Chauchat, E. Schall, M. Mory, M. de la Llave Plataand V. Couaillier (UFR Scienceset Techniques de Pau / Onera)

JAGUAR: a new CFD code dedicated to massively parallel high-order LES computations on complex geometryA. Cassagne, J.-F. Boussuge,G. Puigt, N. Villedieu andA. Genot (CERFACS)

12:15 Lattice-Boltzmann simulationof vortex generatorson a high-lift airfoilR. Denis, B. König and E. Fares (EuroXA SARL / Exa GmbH)

Towards numerical simulation of runback ice accretions K. Szilder and E.P. Lozowski (National Research Council / University of Alberta)

Theoretical and numerical analysis of nonconforming grid interface for unsteady flowsJ. Vanharen, G. Puigt andM. Montagnac (CERFACS)

12:45 Separation and reattachmentin laminar hypersonic flowS.L. Gai, A.Khraibut and A.J. Neely (University of New South Wales)

CFD modeling of a space launch during the atmospheric phaseG. Pont, D. Puech, M. Jubera,M. Dramont and P. Brenner(Airbus Defence & Space)

Latest improvements around hybrid grid technique of the elsA CFD software - Application to turbomachineryM. Soismier, L. Castillon, C. Marmignon, M.-C. Le Papeand V. Couaillier (Onera)

13:15 LUNCH

Wind past the “Château des ducs de Bretagne” - © CSTB

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5 14:15 KEYNOTE CONFERENCE N°2: Metrology for future wind tunnel testing needsPatrick Wagner (Onera)

Session 2: Experimental challenges

Session n° 2a: Wind tunnelsand experimental methodsChairperson: Laurent Joly(ISAE – Supaero)

Session n° 2b: Flow control (1)Chairperson: Daniel Caruana (Onera)

Session n° 2c:Fundamental testings (1)Chairperson: William S. Saric(Texas A&M University)

15:00 Lattice-Boltzmann methodfor Large Eddy Simulationof the flow around a NACA0015 airfoil at high incidenceG. Wissocq, N. Gourdain,A. Eyssartier and O. Malaspinas(ISAE Supaero / Altran / Universityof Geneva)

Experimental and numerical characterization of a plasma synthetic jetF. Laurendeau, F. Chedevergne,O. Léon and G. Casalis (Onera)

Fluctuating pressure measurements in a turbulent separating and reattaching flowJ. Trünkle, A. Mohammed-Taifour and J. Weiss (École de Technologie Supérieure de Montréal)

15:30 Calculation and experimental investigations of transonic wind tunnel perforated walls effect on model test results P.V. Savin (TsAGI)

Experimental and numerical investigation of the interaction of a plasma synthetic jet actuator and a subsonic jet flowF. Chedevergne and O. Léon(Onera)

Numerical simulation and analysis of two-elements wingsailA. Fiumara, N. Gourdain,V. Chapin, J. Senter (ISAE DAEP/ ISAE, University of Toulouse / Assystem France)

16:00 Experimental challenges in a high-Reynolds-number, high-dynamic-pressure, supersonic wind-tunnel facilityÐ. Vukovic, D. Damljanovic, D. Curcic and J. Isakovic (VTI / College of Applied Engineering Studies)

Self adaptive control of the turbulent wake of a square cylinder N. Mazellier, A. Feuvrier andA. Kourta (PRISME Laboratory)

Dynamics of a laminar shock/boundary layer interaction at M=1.6 using experimental and stability approachesN. Bonne, P. Molton, R. Burand V. Brion (Onera)

16:30 COFFEE BREAK

17:00 An overview of HyFIE technical research project: cross testing in main european hypersonic wind-tunnels on EXPERT bodyJ.-P. Brazier (Onera)

Deep stall characterization and identification algorithm on a T-tail aircraft modelL. Hétru, T.M. Faure, S. Kolband O. Montagnier (French Air Force Academy)

Subsonic area rule utilization for high velocity business jet designA.L. Bolsunovsky, N.P. Buzoverya and I.L. Chernyshev (TsAGI)

17:30 Assessment of stochastic estimation ability to reconstruct velocity fieldsA. Arnault, J. Dandois, J. Delva,J.-C. Monnier and J.-M. Foucaut(Onera/Ecole Centrale de Lille)

Meshing for hight-performanceCFD analysis by using automated partitions constructed with the 3Dmedial objectH. Bucklow (TranscenData Europe)

Vortex dynamics resulting from the interaction between two NACA 23 012 airfoils T.M. Faure, L. Hétruand O. Montagnier (French Air Force Academy)

18:00 Experimental study of jet flow injected into a supersonic streamF. Jia, Y. Shi-He, W. Xiao-Hu,G. Dun-Dian and H. Lin(National University of Defense Technology)

Electrohydrodynamic thruster for spatial propulsion: theoretical and experimental characterization of the force produced by a corona dischargeE. Moreau and N. Benard (PPRIME Institute)

18:30 END OF SESSION

SOCIAL EVENT

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5 08:30 KEYNOTE CONFERENCE N°3: Interactions of step-excrescences and crossflow on swept-wingsHelen Reed (Texas A&M University)

Session n°3: New technologies

Session 3a: Laminarity and transitionChairperson: Daniel Arnal (ISAE - Supaero)

Session 3b: Flow control (2)Chairperson: Eric Coustols (Onera)

09:15 Effects of local conditions on step-excrescence induced laminar-turbulent transitionB.K. Crawford, G.T. Duncan Jr., M. W. Tufts, W.S. Saric and H.L. Reed (Texas A&M University)

Unsteadiness characterization and control in turbulent flows with linear stability analysesD. Sipp, C. Mettot, F. Renac (Onera)

09:45 Experimental and numerical study of the effect of gaps on the laminar-turbulent transition of two-dimensional and three-dimensional incompressible boundary layersM. Forte, J. Perraud, S. Beguet, L. Gentili and G. Casalis (Onera)

Influence of a plasma actuator on aerodynamic efforts over a flat plate interacting with a rarefied Mach 2 flowS. Coumar, R. Joussot, V. Lago and J.-D. Parisse(ICARE Institute / Université de Provence/Université de la Méditerranée)

10:15 A Mach 0 to 4 laminar-turbulent transition criterionJ. Perraud and D. Arnal (Onera)

Theoretical investigation of leading edge tubercles on high lift device performanceV. Bhatt, R. Rehmatullah, A. Abdu, U. Arshad,F. Alesayi, B. Mohammed, S. Manassi, and Y.H. Kim (Emirates Aviation University)

10:45 COFFEE BREAK

11:15 Prediction of laminar/turbulent transition in an unstructured finite element Navier-Stokes solver using a boundary-layer codeR. Gross, J.-C. Courty, D. Tran, M., D. Arnal and O. Vermeersch (Dassault Aviation / Onera)

Development of an innovative active flow control system for CROR power plant noise reduction through pylon wake mitigationY. Bury, A. Bordron, H. Belloc and D. Prat (ISAE-Supaero / Aeroconseil / Airbus Operation SAS)

11:45 Systems driven HLFC designT. Backer Dirks and C.J. Atkin (City University London)

Large Eddy Simulation of a flow control device for noise reduction due to a CROR/pylon interactionN. Gourdain, Y. Bury, J. Bodart and L. Dupont(ISAE-Supaero)

12:15 On the turbulent boundary layer at the leading edge of a swept wingE.R. Gowree and C.J. Atkin (City University London)

Experimental and numerical study of Dielectric Barrier Discharge plasma actuation on a Blasius boundary layerN. Szulga, O. Vermeersch, M. Forte and G. Casalis(Onera)

12:45 LUNCH

Surface flow induced by vortex generators - © Onera © ISAE subsonic wind tunnel

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5 14:00 KEYNOTE CONFERENCE N°4: Aerodynamics in Airbus during early program phase: Progress of “Target Setting”Serge Bonnet (Airbus)

Session n°4: New configurations

Session n° 4a: AircraftChairperson: Yannick Caillabet (Airbus)

Session n° 4b: Land vehiclesChairperson: Vincent Herbert (PSA Peugeot Citroën)

Session n° 4c: Rotating bodiesChairperson: Jean-Marc Moschetta (ISAE – Supaero)

14:45 The studies on laminar wings for regional and short range aircraftA.L. Bolsunovsky, N.P. Buzoveryaand N. Pushilin (TsAGI)

A study of the ground influence on the wake of an Ahmed body profile S. Pellerin and B. Podvin (Université Paris-Sud / LIMSI-CNRS)

Experimental and numerical analysis of quiet MAV rotorsC. Nana, J.-M. Moschetta, E. Bénard, S. Prothin and T. Jardin(ISAE- Supaero)

15:15 Experimental and computational analysis of the vortical flow past a simplified model of an engine/pylon/wing installation at low velocity/moderate incidence flight conditionsM. Lucas, Y. Bury, L. Joly and C. Bonnaud (ISAE-Supaero / Airbus Operation SAS)

Underbody aerodynamics of road lorriesR.G. Stephens and H. Babinsky(Cambridge University)

Aerodynamic and acoustic analysis of main rotor blade tips in hover L.I. Garipova, A.S. Batrakov, A.N. Kusyumov, S.A. Mikhailov and G. Barakos (Kazan National Research Technical University / University of Liverpool)

15:45 COFFEE BREAK

16:15 Transonic shock wave boundary layer interaction of normal shock around a supercritical airfoil at high Reynolds numberD. Szubert, F. Grossi, I. Asproulias, Y. Hoarau and M. Braza(IMFT / Embraer / ICUBE)

Flow control devices for drag reduction and down force of a detailed road vehicle model R. Placzek, P. Scholz and C. Othmer (Technische Universität Braunschweig / Volkswagen AG)

Numerical impact of transition on profile wakes and BWI applicationsG. Delattre, J.-P. Lackand F. Falissard (Onera)

16:45 Numerical investigations of aerodynamic properties of a propeller blown circulation control system on a high wing aircraftD. Keller and R. Rudnik (DLR)

Wake structure and drag of vehicles with rounded rear edgesG. Rossitto, J. Borée, C. Sicot, V. Ferrand and F. Harambat (PSA Peugeot Citroën / PPRIME Institute / ISAE-Supaero)

Aerodynamic loads fluctuations alleviation by circulation control on wind turbine blades S. Aubrun, A. Leroy andP. Devinant (PRISME Laboratory)

17:15 The “Frigate Ecojet”: a new widebody middle-range aircraft with oval fuselage cross sectionV.I. Birjuk, A.L. Bolsunovsky,N.P. Buzoverya, V.I. Chernousov, Yu.S. Mikhailov and E.A. Pigusov (TsAGI)

Active control applied to the flow past a backward facing ramp: S-PIV measurements and POD analysisD. Hlevca, P. Gilliéron and F. Grasso (CNAM-IAT / DynFluid Laboratory)

Integrating CFD into wind tunnel testing of a shrouded wind turbineM. Karczewski, K. Sobczak, M. Kulak, K. Olasek and K. Jozwik (Lodz University of Technology)

17:45 Experimental and computational study of the low-speed aerodynamic performance of an unmanned combat air vehicle in yawed flightL.J. Johnston (University of Salford)

Drag-coefficient behavior for five bio-inspired high speed train designsS. Linic, B. Rasuo, M. Kozic, V. Lucanin and A. Bengin (Institute Gosa / University of Belgrade / Military Technical Institute)

Wind tunnel experimental investigation of diffuser augmented wind turbine model K. Olasek, M. Karczewski,M. Lipian and K. Józwik (Lodz University of Technology)

18:30 END OF SESSIONS

The 2015 Lanchester Lecture organized by the Royal Aeronautical SocietyAn overview of flow control activities at Dassault Aviation for the last 25 years by Jean-Pierre Rosenblum

20:00 AWARD OF THE 3AF INTERNATIONAL CONFERENCE ON APPLIED AERODYNAMICSAND BANQUET

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5 08:45 KEYNOTE CONFERENCE N° 5: Rotary wing aerodynamics - recent progress and future challengeGeorge Barakos (University of Liverpool)

Session n°5: Multiphysics and optimization

Session n°5a: Cavity and jet flowsChairperson: Yannick Caillabet (Airbus)

Session n°5b: OptimizationChairperson: Chris J. Atkin (City University London)

09:30 Effects of internal structures on unsteady cavity flows K. Knowles, M.V. Finnis and L.D. Sapsford(Cranfield University)

A multi-point performance matched aerofoil design algorithm for a scaled wind turbine rotor modelS. Martin and A.H. Day (University of Strathclyde)

10:00 Transient aerodynamics and aeroacoustics of complex-geometry weapon baysD. Bacci, A.J. Saddington and D. Bray(Cranfield University)

Numerical and modeling issues for optimizationof flow control devicesR. Duvigneau, J. Labroquère and E. Guilmineau (INRIA Sophia-Antipolis / LHEEA-Ecole Centralede Nantes)

10:30 COFFEE BREAK

11:00 High-order and subgrid model effects on finite element DES-LES computations of a transonic cavity experimentP. Yser, S. Barré, F. Chalot and F. Dagrau(Dassault Aviation)

Experimental optimization by genetic algorithm for flow separation control with surface plasma actuatorN. Benard, J. Pons-Prats, J. Periaux, G. Bugeda, J.-P. Bonnet and E. Moreau (PPRIME Institute / CIMNE/Universitat Politècnica de Catalunya)

11:30 Non viscous sensitivity analysis of noise generation mechanism in a low Mach number jet C. Airiau and T. Ansaldi (IMFT / University of Toulouse)

Discrete adjoint method for shape optimization and mesh adaptation in the elsA code. Statusand challengesJ. Peter, F. Renac, A. Dumont and M. Méheut (Onera)

12:00 Modal analysis of near-field pressure fluctuationfor a cold subsonic jet J.-P. Brazier, M. Huet, O. Léon and M. Itasse (Onera)

Innovative aerodynamic design procedurefor a forward-swept wing in preliminary design A. Viti, A. Dumont, G. Carrier and R. Hewson(Onera / Imperial College London)

12:30 Shock-cell noise of supersonic under-expanded jetsC. Pérez Arroyo, G. Daviller, G. Puigt and C. Airiau(CERFACS)

Recent advances in the integration of CFDinto the missile design process M. Dodds, S. Lawson and N. Taylor (MBDA UK)

13:00 LUNCH

14:30 TECHNICAL VISIT

17:00END OF CONFERENCE

Reg

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ISAE, Campus SUPAERO, Complexe Scientifique de Rangueil10, Avenue Edouard Belin - 31400 TOULOUSE – France

SECURITY

Access to technical visit (Airbus) can only be granted upon former registration before March, 2nd 2015. ID or passport copy must be attached to registration.For security reasons, checks will be organized systematically at the entrance of the visit.Please be reminded that your ID will be requested. You shall not be allowed to participate without valid ID.

LANGUAGE

Offical language for the conference is English.

REGISTRATION

Delegates including Chairmen and Speakers are requested to register and settle registration feesprior 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 31 March 2015, access to the technical visit and Conference Proceedings. All prices quoted are in EURO. Registration fees not subject to VAT.

3AF Individual Member € 650.00Speaker/Chairman € 650.00Participant € 900.00Academics/Student/PhD € 400.00

Additional conference banquetticket for accompanying person € 60.00

EDUCATION COURSE

Possibility to register for a continuing education course. For more information, please contact our partner EUROSAE Valérie Pineau - Email: [email protected] - Phone : +33 (0)1 41 08 01 01 - Fax: +33 (0)1 41 08 07 77

REGISTRATION FORM AND PAYMENT

On line registration on: http://aero2015.evenium.netComplete online form and follow payment indication. Upon receipt of your payment an invoiceand 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, € 350 cancellation fee will apply to participants,speakers and chairmen, € 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.

SECRETARIAT

For more information please contact :

3AF Executive Secretariat - 6, Rue Galilée – 75016 Paris, France - Fax : +33 (0)1 56 64 12 31Anne Venables - E-mail: [email protected] – Phone : +33 (0)1 56 64 12 30Aude Lurbe - E-mail : [email protected] – Phone : +33 (0)1 56 64 12 37


50th edition of the 3AF International Conference on Applied Aerodynamics, Toulouse, March 30, 31, April 1, 2015P

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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,

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• 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.

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 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.

CD-adapco is the world’s largest independent CFD focused provider of engineering simulation software, support and services. We have over 30 years of experience in delivering industrial strength engineering simulation. The scope of our activities extends well beyond software development to encompass a wide range of CAE engineering services in both CFD and FEA.

We have over 8000 users of our software, working at 3000 different companies, spending over $181 million on our software and services. Our customer approval ratings are very high; in our last customer survey 93% of our customers declared themselves satisfied, or very satisfied with our software and services, a fact reflected in a consistently high customer retention rate.

Consistently growing at an organic rate of over 15% per year, CD-adapco employs over 850 talented individuals, working at 30 offices around the globe, involved in dedicated support, software development and engineering services.

CD-adapco is the world’s largest independent CFD focused provider of engineering simulation software, support and services. We have over 30 years of experience in delivering industrial strength engineering simulation. The scope of our activities extends well beyond software development to encompass a wide range of CAE engineering services in both CFD and FEA.

We have over 8000 users of our software, working at 3000 different companies, spending over $181 million on our software and services. Our customer approval ratings are very high; in our last customer survey 93% of our customers declared themselves satisfied, or very satisfied with our software and services, a fact reflected in a consistently high customer retention rate.

Consistently growing at an organic rate of over 15% per year, CD-adapco employs over 850 talented individuals, working at 30 offices around the globe, involved in dedicated support, software development and engineering services.

Airbus is the world’s leading commercial aircraft manufacturer whose customer focus, commercial know-how, technological leadership and manufacturing efficiency have set the standard for the aviation industry.

Airbus’ comprehensive product line comprises highly successful families of aircraft ranging from 100 to more than 500 seats: the single-aisle A320 Family (including A320neo, the best-selling aircraft in aviation history); the widebody, long-range A330 Family (including the A330-200 Freighter, the A330-based MRTT, and now the recently launched A330-800neo and -900neo); the next generation A350 XWB Family; and the flagship A380.

Ensuring the company’s full range of jetliners remains at the cutting edge of performance, Airbus is continuously developing product innovations to meet its customers’ needs. Airbus’ unique approach across all its fly-by-wire aircraft families results in the highest possible degree of commonality in airframes, on-board systems, cockpits and handling characteristics, which significantly reduces airlines’ operating costs.

Dedicated to remaining close to its global customer base, Airbus supports its high-quality, safe and reliable in-service fleet with a wide range of customer services, tailored to the needs of individual operators all over the world.

ITI TranscenData is a leader in the delivery of interoperability solutions for CAD/CAM/CAE/PDM. Since 1985 ITI TranscenData has partnered with the leading PLM vendors to assemble an unparalleled suite of software products and services - all aimed at eliminating the non-value-added time and costs associated with reusing product data and maintaining data integrity. ITI TranscenData’s solutions include CADfix, Proficiency, DrawtoPMI, CADIQ and DEXcenter.

CADfix is one of the leading tools for 3D geometry exchange and model preparation, CAD-CAE application integration, and process automation. CADfix helps analysis engineers prepare 3D CAD models for different CFD, FEA and CEM applications using an extensive set of configurable geometry repair, simplification and conditioning tools. The highly customisable CADfix architecture enables the integration of external best-in-class meshing and analysis applications into the CADfix environment.

CADfix generates models that are more suitable for CAE, enabling reduced model rework, improved meshability, reduced analysis lead times, and providing a greater opportunity for optimised analysis lead design processes. CADfix is deployed throughout the aerospace supply chain and has enabled significant customer success through greater application integration and process automation.


The conference will take place in the ISAE, Campus SUPAERO.

Getting to ISAE

Loca

tion

ISAE, Campus SUPAERO,Complexe Scientifique de RANGUEIL10 avenue Edouard Belin31400 Toulouse, FranceGPS: Latitude N 43° 34’ 00’’Longitude E 1° 28’ 29’’

For detailed access:

http://supaero.isae.fr//fr/acces_au_campus_supaero.html

Acc

omm

odat

ion

Hotel Ours Blanc Wilson **** 2, Rue Victor Hugo - 31000 TOULOUSE

Tel: +33 (0) 5 61 21 62 40 - Fax: +33 (0) 5 61 23 62 34

E-mail: [email protected]

Citiz Hotel ****18, Allées Jean Jaurès - 31000 TOULOUSE

Tel: +33 (0) 5 61 11 18 18 - Fax : +33 (0) 5 31 61 61 41


Hotel Ours Blanc Centre ***14, Place Victor Hugo - 31000 TOULOUSE

Tel: +33 (0) 5 61 21 25 97 - Fax: +33 (0) 5 61 23 96 27


Please contact the Executive Secretary for information:

Anne Venables - 6, rue Galilée - 75016 Paris, France

Tél +33 (0)1 56 64 12 30 - [email protected]

Hotel Père Léon ***2, Place Esquirol - 31000 TOULOUSE

Tel : +33 (0) 5 61 21 70 39


IBIS Styles ***13, Boulevard Bonrepos - 31000 TOULOUSE

Tel : +33 (0) 5 61 62 44 78 - Fax : +33 (0) 5 61 63 18 06

E-mail : [email protected]

Make your reservation as soon as possible.

Complete list hotels in Toulouse:http://www.so-toulouse.com/organiser-sa-venue/les-acteurs-par-categorie/hebergements.html

We recommended hotels in the center of Toulouse. Shuttles will be organized to ISAE.

Hotel close to the Conference:

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: Challenges in flow

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ew technologies

Session 5

: Multip

hysics and op

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Session 1

a

Flowseparation

Session 1

b

Com

plexflow

s

Session 1

c

Methodo-logies

Session 3

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Laminarity and

transition

Session 3

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Flow control(2

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Cavity and jet flow

s

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Optim

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LunchLunch

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Wind

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ethods

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Flow control(1

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Fundamental

testings

Session 4

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Aircraft

Session 4

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Landvehicles

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international conference on applied aerodynamics ... of the 3af international conference on applied...

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