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PROGRAMME
50 edition of the 3AF
th
International Conference on
Applied Aerodynamics
Forthcoming Challenges
for Aerodynamics
Toulouse, France – March 30, 31, April 1, 2015
http://3af-aerodynamics2015.com
« Convertible configuration. Computation - © ONERA »
Scientific Committee
50th edition of the 3AF International Conference on Applied Aerodynamics, Toulouse, March 30, 31, April 1, 2015
Holger BABINSKY
Abderrahmane BAÏRI
Emmanuel BÉNARD
Jean-Paul BONNET
Jacques BORÉE
Pierre BRENNER
Stéphane BURGUBURU
Yannick BURY
Laurent CAMBIER
Bruno CHANETZ
Paola CINNELLA
Jean COLLINET
Michel COSTES
Jean COUSTEIX
Denis DARRACQ
Jean DÉLERY
Philippe DEVINANT
Piotr DOERFFER
Michel DUMAS
Anne GAZAIX
Nicolas GÉTIN
Patrick GILLIÉRON
Patrick GNEMMI
Francesco GRASSO
Vincent HERBERT
Denis JEANDEL
Emilie JÉRÔME
Azeddine KOURTA
Viviana LAGO
Hadrien LAMBARÉ
Olivier ORLANDI
Didier PAGAN
Sandrine PALERM
Pierre-Yves PAMART
Jean-Denis PARISSE
Joël RENEAUX
Jean-Pierre ROSENBLUM
William S. SARIC
Jean TENSI
University of Cambridge
University of Paris West
ISAE
University of Poitiers
ISAE - ENSMA
Airbus Defence and Space
Safran Snecma
ISAE
ONERA
ONERA
Arts et Métiers ParisTech
Airbus Defence and Space
ONERA
ISAE
Airbus
3AF and ONERA
University of Orléans
Polish Academy of Sciences
Safran Snecma
Airbus
MBDA
Renault
ISL
IAT - CNAM
PSA Peugeot Citroën
Ecole Centrale de Lyon
DGA
University of Orléans
CNRS
CNES
Safran Herakles
MBDA
CNES
Safran Snecma
University of Aix-Marseille
ONERA
Dassault Aviation
Texas A&M University
3AF
50 edition of the 3AF
th
International Conference on
Applied Aerodynamics
Forthcoming Challenges
for Aerodynamics
Toulouse, France
March 30, 31, April 1, 2015
High-speed flow control - © ISL
www.3af-aerodynamics2015.com
50th edition of the 3AF International Conference on Applied Aerodynamics, Toulouse, March 30, 31, April 1, 2015
Forthcoming Challenges for Aerodynamics
The 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 windturbines, 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, etc.
Programme overview
Flow simulation past an automobile © ONERA
MONDAY 30 MARCH 2015
08:00
09:00
09:30
10:15
14:15
15:00
Registration
Conference Welcome
Keynote Conference N°1
Session n°1: Challenges in flow modelling and numerical simulation
Keynote Conference N°2
Session n°2: Experimental Challenges
TUESDAY 31 MARCH 2015
08:30
09:15
14:00
14:45
18:30
20:15
Keynote Conference N°3
Session n°3: New technologies
Keynote Conference N°4
Session n°4: New configurations
The 2015 Lanchester Lecture, organized by the Royal Aeronautical Society
Award of the 3AF International Conference on Applied Aerodynamics and Banquet
WEDNESDAY 1 APRIL 2015
08:45
09:30
14:30
17:00
Keynote Conference N°5
Session n°5: Multiphysics and optimization
Technical visit: Airbus
End of conference
CONFERENCE LOCATION:
ISAE - SUPAERO
Complexe Scientifique de RANGUEIL
10 avenue Edouard Belin
31400 Toulouse, France
ORGANIZATION:
Monday, March 30, 2015
50th edition of the 3AF International Conference on Applied Aerodynamics, Toulouse, March 30, 31, April 1, 2015
ROOM 1
09:00
CONFERENCE WELCOME
Michel Scheller (President, French Aeronautics and Astronautics Society)
Olivier Lesbre (Director, Institut Supérieur de l’Aéronautique et de l’Espace)
ROOM 1
09:30
KEYNOTE CONFERENCE N°1:
Turbulence prediction in aeronautics and neighboring fields
Philippe Spalart (Boeing Company)
Session n° 1: Challenges in flow modelling and numerical simulation
ROOM 1
ROOM 2
ROOM 3
Session n° 1a: Flow separation
Chairperson: Jean-Fra nçois
Boussuge (CERFACS)
Session n° 1b: Complex flows
Chairperson: Alain Merlen
(ONERA)
Session n° 1c: Methodologies
Chairperson: Jean-Marie
Le Gouez (ONERA)
10:15
Application of a hybrid variational
multiscale model to massively
separated flows
E. Itam, S. Wornom, B. Koobus and
A. Dervieux (University of Montpellier /
LEMMA / INRIA-Sophia Antipolis)
Body force modeling for
efficient analysis of intake-fan
interactions
E. William, W. Thollet, F. Blanc,
G. Dufour and X. Carbonneau
(Airbus Operations SAS/ISAE-Supaero)
A Contribution to the way
of the all-Mach number
N. 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 wing
E. Guilmineau, M. Visonneau and
S. Toxopeus (LHEEA-Ecole Centrale
de Nantes / MARIN-Wageningen)
Parallel anisotropic 3D mesh
adaptation for unsteady
turbulent flows
E. Hachem, L. Billon, J. Sari,
F. Cauneau and Y. Mesri
(MINES - ParisTech)
Instabilities in helical vortex
systems: linear analysis and
nonlinear dynamics
C. Selçuk, I. Delbende
and M. Rossi (LIMSI-CNRS /
University Pierre et Marie Curie)
11:15
COFFEE BREAK
11:45
Mach number effects on
buffeting flow on a half
wing-body configuration
F. Sartor and S. Timme
(University of Liverpool)
Study of a cooling device
of confined impacting air jets
on a heating cylinder
N. Chauchat, E. Schall,
M. Mory, M. de la Llave Plata
and V. Couaillier (UFR Sciences
et Techniques de Pau / ONERA)
JAGUAR: a new CFD code
dedicated to massively parallel
high-order LES computations
on complex geometry
A. Cassagne, J.-F. Boussuge,
G. Puigt, N. Villedieu and
A. Genot (CERFACS)
12:15
Lattice-Boltzmann simulation
of vortex generators
on a high-lift airfoil
R. Denis, B. König, E. Fares and
A. Ribeiro (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 flows
J. Vanharen, G. Puigt and
M. Montagnac (CERFACS)
12:45
Separation and reattachment
in laminar hypersonic flow
S.L. Gai, A.Khraibut and A.J. Neely
(University of New South Wales)
CFD modeling of a space
launch during the atmospheric
phase
G. 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 turbomachinery
M. Soismier, L. Castillon,
C. Marmignon, M.-C. Le Pape
and V. Couaillier (ONERA)
13:15
LUNCH
Wind past the “Château des ducs de Bretagne” - © CSTB
Monday, March 30, 2015
50th edition of the 3AF International Conference on Applied Aerodynamics, Toulouse, March 30, 31, April 1, 2015
ROOM 1
14:15
KEYNOTE CONFERENCE N°2:
Metrology for future wind tunnel testing needs
Patrick Wagner (ONERA)
Session 2: Experimental challenges
ROOM 1
ROOM 2
ROOM 3
Session n° 2a: Wind tunnels
and experimental methods
Chairperson: 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 method
for Large Eddy Simulation
of the flow around a NACA0015
airfoil at high incidence
G. Wissocq, N. Gourdain,
A. Eyssartier and O. Malaspinas
(ISAE Supaero / Altran / University
of Geneva)
Experimental and numerical
characterization of a plasma
synthetic jet
F. Laurendeau, F. Chedevergne,
O. Léon and G. Casalis (ONERA)
Fluctuating pressure
measurements in a turbulent
separating and reattaching flow
J. 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 flow
F. Chedevergne and O. Léon
(ONERA)
Numerical simulation and
analysis of two-elements
wingsail
A. Fiumara, N. Gourdain,
V. Chapin, J. Senter (ISAE DAEP/
ISAE, University of Toulouse /
Assystem France)
16:00
Experimental challenges in a
high-Reynolds-number, highdynamic-pressure, supersonic
wind-tunnel facility
Ð. Vukovi´c, D. Damljanovi´c,
´ cic´ and J. Isakovi´c
D. Curˇ
(VTI / College of Applied
Engineering Studies)
Self adaptive control of the
turbulent wake of a square
cylinder
N. Mazellier, A. Feuvrier and
A. Kourta (PRISME Laboratory)
Dynamics of a laminar shock/
boundary layer interaction at
M=1.6 using experimental and
stability approaches
N. Bonne, P. Molton, R. Bur
and V. Brion (ONERA)
16:30
COFFEE BREAK
17:00
An overview of HyFIE technical
research project: cross testing in
main european hypersonic windtunnels on EXPERT body
J.-P. Brazier (ONERA)
Deep stall characterization and
identification algorithm on a
T-tail aircraft model
L. Hétru, T.M. Faure, S. Kolb
and O. Montagnier
(French Air Force Academy)
Subsonic area rule utilization
for high velocity business jet
design
A.L. Bolsunovsky, N.P. Buzoverya
and I.L. Chernyshev (TsAGI)
17:30
Assessment of stochastic
estimation ability to reconstruct
velocity fields
A. Arnault, J. Dandois, J. Delva,
J.-C. Monnier and J.-M. Foucaut
(ONERA/Ecole Centrale de Lille)
Meshing for hight-performance
CFD analysis by using
automated partitions
constructed with the 3D
medial object
H. Bucklow (TranscenData Europe)
Vortex dynamics resulting
from the interaction between
two NACA 23 012 airfoils
T.M. Faure, L. Hétru
and O. Montagnier
(French Air Force Academy)
18:30
WELCOME COCKTAIL, HOSTED BY MAIRIE DE TOULOUSE
20:00
END OF DAY 1
Blended wing body. Calculation © ONERA
Tuesday, March 31, 2015
50th edition of the 3AF International Conference on Applied Aerodynamics, Toulouse, March 30, 31, April 1, 2015
ROOM 1
08:30
KEYNOTE CONFERENCE N°3:
Interactions of step-excrescences and crossflow on swept-wings
Helen Reed (Texas A&M University)
Session n°3: New technologies
ROOM 1
ROOM 2
Session 3a: Laminarity and transition
Chairperson: 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 transition
B.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 analyses
D. Sipp, C. Mettot, F. Renac (ONERA)
09:45
Experimental and numerical study of the effect of
gaps on the laminar-turbulent transition of twodimensional and three-dimensional incompressible
boundary layers
M. 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 flow
S. 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 criterion
J. Perraud and D. Arnal (ONERA)
Theoretical investigation of leading edge tubercles
on high lift device performance
V. 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 code
R. 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 mitigation
Y. Bury, A. Bordron, H. Belloc and D. Prat
(ISAE-Supaero / Aeroconseil / Airbus Operation SAS)
11:45
Systems driven HLFC design
T. 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 interaction
N. Gourdain, Y. Bury, J. Bodart and L. Dupont
(ISAE-Supaero)
12:15
On the turbulent boundary layer at the leading
edge of a swept wing
E.R. Gowree and C.J. Atkin (City University London)
Experimental and numerical study of Dielectric
Barrier Discharge plasma actuation on a Blasius
boundary layer
N. Szulga, O. Vermeersch, M. Forte and G. Casalis
(ONERA)
12:45
LUNCH
Surface flow induced by vortex generators - © ONERA
© ISAE subsonic wind tunnel
Tuesday, March 31, 2015
50th edition of the 3AF International Conference on Applied Aerodynamics, Toulouse, March 30, 31, April 1, 2015
ROOM 1
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
ROOM 1
ROOM 2
ROOM 3
Session n° 4a: Aircraft
Chairperson: Yannick Caillabet
(Airbus)
Session n° 4b: Land vehicles
Chairperson: Vincent Herbert
(PSA Peugeot Citroën)
Session n° 4c: Rotating bodies
Chairperson: Nicolas Gourdain
(ISAE – Supaero)
14:45
The studies on laminar wings for
regional and short range aircraft
A.L. Bolsunovsky, N.P. Buzoverya
and 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 rotors
C. 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
conditions
M. Lucas, Y. Bury, L. Joly and
C. Bonnaud (ISAE-Supaero / Airbus
Operation SAS)
Underbody aerodynamics of
road lorries
R.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 number
D. Szubert, F. Grossi, I. Asproulias,
Y. Hoarau and M. Braza
(IMFT / Embraer / ICUBE)
Wake structure and drag of
vehicles with rounded rear
edges
G. Rossitto, J. Borée, C. Sicot,
V. Ferrand and F. Harambat
(PSA Peugeot Citroën / PPRIME
Institute / ISAE-Supaero)
Numerical impact of transition
on profile wakes and BWI
applications
G. Delattre, J.-P. Lack
and F. Falissard (ONERA)
16:45
Numerical investigations of
aerodynamic properties of a
propeller blown circulation
control system on a high wing
aircraft
D. Keller and R. Rudnik (DLR)
Active control applied to the
flow past a backward facing
ramp: S-PIV measurements
and POD analysis
D. Hlevca, P. Gilliéron
and F. Grasso (CNAM-IAT /
DynFluid Laboratory)
Aerodynamic loads fluctuations
alleviation by circulation control
on wind turbine blades
S. Aubrun, A. Leroy and
P. Devinant (PRISME Laboratory)
17:15
The “Frigate Ecojet”: a new
widebody middle-range aircraft
with oval fuselage cross section
V.I. Birjuk, A.L. Bolsunovsky,
N.P. Buzoverya, V.I. Chernousov,
Yu.S. Mikhailov and E.A. Pigusov
(TsAGI)
Experimental optimization
by genetic algorithm for flow
separation control with surface
plasma actuator
N. Benard, J. Pons-Prats, J. Periaux,
G. Bugeda, J.-P. Bonnet and
E. Moreau (PPRIME Institute /
CIMNE/Universitat Politècnica
de Catalunya)
Integrating CFD into wind tunnel
testing of a shrouded wind
turbine
M. Karczewski, K. Sobczak,
´
M. Kulak, K. Olasek and K. Józwik
(Lodz University of Technology)
17:45
Experimental and computational
study of the low-speed
aerodynamic performance of an
unmanned combat air vehicle in
yawed flight
L.J. Johnston (University of Salford)
Wind tunnel experimental
investigation of diffuser
augmented wind turbine model
K.Olasek, M.Karczewski, M.Lipian,
´
P.Wiklak and K. Józwik
(Lodz University of Technology)
18:30
The 2015 Lanchester Lecture organized by the Royal Aeronautical Society, RAeS
An overview of flow control activities at Dassault Aviation for the last 25 years by Jean-Pierre Rosenblum
20:15
AWARD OF THE 3AF INTERNATIONAL CONFERENCE ON APPLIED AERODYNAMICS
AND BANQUET, TOULOUSE
23:00
END OF DAY 2
Wednesday, April 1, 2015
50th edition of the 3AF International Conference on Applied Aerodynamics, Toulouse, March 30, 31, April 1, 2015
ROOM 1
08:45
KEYNOTE CONFERENCE N° 5:
Rotary wing aerodynamics - recent progress and future challenge
George Barakos (University of Liverpool)
Session n°5: Multiphysics and optimization
ROOM 1
ROOM 2
Session n°5a: Cavity and jet flows
Chairperson: Laurent Jacquin (ONERA)
Session n°5b: Optimization
Chairperson: 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 model
S. Martin and A.H. Day (University of Strathclyde)
10:00
Transient aerodynamics and aeroacoustics of
complex-geometry weapon bays
D. Bacci, A.J. Saddington and D. Bray
(Cranfield University)
Numerical and modeling issues for optimization
of flow control devices
R. Duvigneau, J. Labroquère and E. Guilmineau
(INRIA Sophia-Antipolis / LHEEA-Ecole Centrale
de Nantes)
10:30
COFFEE BREAK
11:00
High-order and subgrid model effects on finite
element DES-LES computations of a transonic
cavity experiment
P. Yser, S. Barré, F. Chalot and F. Dagrau
(Dassault Aviation)
Innovative aerodynamic design procedure for a
forward-swept wing in preliminary design
A. Viti, A. Dumont, G. Carrier and R. Hewson
(ONERA / Imperial College London)
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. Status
and challenges
J. Peter, F. Renac, A. Dumont and M. Méheut (ONERA)
12:00
Modal analysis of near-field pressure fluctuation
for a cold subsonic jet
J.-P. Brazier, M. Huet, O. Léon and M. Itasse
(ONERA)
Electrohydrodynamic thruster for spatial
propulsion: theoretical and experimental
characterization of the force produced
by a corona discharge
E. Moreau and N. Benard (PPRIME Institute)
12:30
Shock-cell noise of supersonic under-expanded jets
C. Pérez Arroyo, G. Daviller, G. Puigt and C. Airiau
(CERFACS)
Recent advances in the integration of CFD
into the missile design process
M. Dodds, S. Lawson and N. Taylor (MBDA UK)
13:00
LUNCH
14:30
TECHNICAL VISIT : AIRBUS ASSEMBLY PLANT, TOULOUSE
17:00
END OF CONFERENCE
Registration
50th edition of the 3AF International Conference on Applied Aerodynamics, Toulouse, March 30, 31, April 1, 2015
CONFERENCE VENUE
ISAE, Campus SUPAERO, Complexe Scientifique de Rangueil
10, 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 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 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
Speaker/Chairman
Participant
Academics/Student/PhD
€
€
€
€
650.00
650.00
900.00
400.00
Additional conference banquet
ticket 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.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, € 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 31
Anne Venables - E-mail: [email protected] – Phone : +33 (0)1 56 64 12 30
Aude Lurbe - E-mail : [email protected] – Phone : +33 (0)1 56 64 12 37
Partners
50th edition of the 3AF International Conference on Applied Aerodynamics, Toulouse, March 30, 31, April 1, 2015
The “Institut Supérieur de l’Aéronautique et de l’Espace”
(ISAE) was created in 2007 from the merger of the two
prestigious French “Grandes Ecoles”: SUPAERO (1909)
and ENSICA (1945). ISAE is today, a worldwide reference in
aerospace higher education and research.
The Institute provides high-level Graduate Programs in
engineering (SUPAERO and ENSICA), Master’s degrees,
Postgraduate Specialized Masters, PhD degrees, with a
wide range of career opportunities: engineering, research
and development, logistics, consulting, finance, etc.
ISAE also develops a very active research policy around four main principles:
• to ensure a strong link between programs and research,
• to set up an international center for hosting and training for Master’s degrees, Specialized
Masters and PhD degrees,
• to guarantee a proper balance between academic visibility and industrial aims proximity,
• to promote innovation in the aerospace field.
Concerning its relations with firms, ISAE is always pursuing adequacy between its educational
objectives and the business needs, with in particular:
• participation in tuitions of many professionals from firms,
• a very wide range of internship offers allowing students to put their knowledge into practice,
• research always turned towards future needs of industry, in the aerospace or high technology field.
At the international level, ISAE cooperates with the best European and North-American universities
with concretely:
• many students and professors exchanges,
• the launch of common education and research programs,
• the active involvement in many networks such as PEGASUS, TIME, PRES “Toulouse University”
or the world-class “Aerospace Valley competitiveness cluster”.
See more at: http://www.isae.fr/
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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.
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.
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 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.
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.
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 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.
A i r b u s i s t h e w o r l d ’s l e a d i n g
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.
EUROSAE is a Public Limited Company, a subsidiary of two
major schools, ISAE, Institut Supérieur de l’Aéronautique et
de l’Espace, ENSTA ParisTech, Ecole Nationale Supérieure
de Techniques Avancées.
The mission is to deliver to engineers, technicians and
executives, a “postgraduate training” which is aimed to update
their professional knowledge and skills. Training courses are
particularly targeted, intensive and short, in order to:
• strengthen or update their knowledge in their field of
activity.
• broaden their knowledge in related areas, especially for a better understanding of
techniques and methods that they will have to know better how to communicate
with their colleagues.
• prepare and/or accompany a development of their position or their career.
EUROSAE offer a wide range of non graduated training courses, some of them are unique in
France, in two major areas:
• Engineer’s techniques and business from high technologies sector.
• Cross activities including: engineering, business management and human resources
management.
Measurement Specialties is a global designer and manufacturer of sensors and sensor-based systems which measure pressure/
force, position, vibration, temperature, humidity, and fluid properties. Our products are used as embedded devices by original
equipment manufacturers (OEMs) or as stand alone sensors for test and measurement to provide critical monitoring, feedback
and control input. We are at the heart of many everyday products and provide a vital link to the physical world.
Our value proposition is to understand your sensing needs and develop a solution that meets your performance and cost
objectives. At Measurement Specialties, we are Sensing Your World. www.meas-spec.com
Location
50th edition of the 3AF International Conference on Applied Aerodynamics, Toulouse, March 30, 31, April 1, 2015
The conference will take place in the Institut Supérieur de l’Aéronautique et de l’Espace (ISAE-SUPAERO).
The Institute provides high-level Graduate Programs in engineering.
ISAE is today, a woldwide reference in aerospace higher education and research.
Getting to ISAE-SUPAERO
ISAE-SUPAERO,
Complexe Scientifique de RANGUEIL
10 avenue Edouard Belin
31400 Toulouse, France
GPS: Latitude N 43° 34’ 00’’
Longitude E 1° 28’ 29’’
Métro B “Ramonville”
+ Bus 68 “Avenue Edouard Belin”
More information:
www.tisseo.fr/
For detailed access:
Accommodation
http://supaero.isae.fr//fr/
acces_au_campus_supaero.html
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-SUPAERO.
Citiz Hotel ****
Hotel Ours Blanc Centre ***
18, Allées Jean Jaurès – 31000 TOULOUSE
Tel: +33 (0) 5 61 11 18 18 – Fax : +33 0 5 31 61 61 41
e-mail: [email protected] - web: http://www.citizhotel.com/
Special rate for AERO 2015 Delegates until March, 2nd
14, Place Victor Hugo – 31000 TOULOUSE
Tel: +33 (0)5 61 21 25 97 – Fax: +33 (0)5 61 23 96 27
e-mail: [email protected]
web: http://www.hotel-oursblanc.com/
Grand Hôtel de l’Opéra ****
1, Place du Capitole – 31000 TOULOUSE
Tel: +33(0)5 61 21 82 66 - e-mail: [email protected]
web : http://www.grand-hotel-opera.com/
Special rate for AERO 2015 Delegates until March, 2nd
Hotel Père Léon ***
2, Place Esquirol – 31000 TOULOUSE
Tel : +33 (0)5 61 21 70 39 - e-mail: [email protected]
web: http://www.pere-leon.com/
Hotel Ours Blanc Wilson ****
Hotel IBIS Toulouse Centre ***
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]
web: http://www.hotel-oursblanc.com/
2, Rue Claire Pauilhac – 31000 TOULOUSE
Tel: +33 (0)5 61 63 61 63 - e-mail: [email protected]
web: http://www.accorhotels.com/fr/
hotel-1429-ibis-toulouse-centre/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 - [email protected]
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MONDAY 30 MARCH 2015
CONFERENCE WELCOME
KEYNOTE CONFERENCE N°1
Session 1a
Complex
flows
Session 1b
Methodologies
Session 1c
Session 1: Challenges in flow modelling
Flow
separation
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TUESDAY 31 MARCH 2015
WEDNESDAY 01 APRIL 2015
Session 3a
Session 5a
Optimization
Session 5b
END OF CONFERENCE
TECHNICAL VISIT
Lunch
Cavity and jet flows
Session 5: Multiphysics and optimisation
KEYNOTE CONFERENCE N°5
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KEYNOTE CONFERENCE N°3
Session 3a
Flow control
(2)
Session 3: New technologies
Laminarity and
transition
Session 4b
Lunch
Session 4b
Lunch
Session 4a
KEYNOTE CONFERENCE N°4
Session 2c
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Aircraft
KEYNOTE CONFERENCE N°2
Session 2b
Fundamental
testings
&
Session 4: New configurations
Session 2a
Flow control
(1)
Rotating
bodies
AWARD AND BANQUET
The RAeS Lanchester Lecture
Land
vehicles
Session 2: Experimental challenges
Wind
tunnels and
experimental
methods
WELCOME COCKTAIL
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Designed by neosema – Printed by ONERA
50th edition of the 3AF International Conference on Applied Aerodynamics, Toulouse, March 30, 31, April 1, 2015