FINAL PROGRAM

8.00 Registration and Welcome Breakfast
9.00 Welcome - Presentation of the conference Program
9.10 SAMTECH 20 years, 10th Users Conferences and AIRBUS successes
E. Carnoy, SAMTECH CEO
9.30 ISAMI, Integration of Structure Analysis for AIRBUS aircrafts
Jocelyn Gaudin, AIRBUS
10.20 COMBOX, optimization and sizing of aircraft composite box structures
Lars Krog, AIRBUS
10.40 Break
11.00 Tolérance aux dommages des structures aéronautiques - Délaminage dans les stratifiés monolithiques et flambage des structures minces
Pascal Thévenet, EADS CCR
11.20 Failure of woven carbon composites: development of a new tool for helicopter applications
Axelle De Gelas, EUROCOPTER
11.40 Multi-scale experimental and numerical analysis of inserts in sandwich structures
Bruno Castanié, IGMT, LMS SUPAERO
12.00 Bird impact on composite structures using EUROPLEXUS
Etienne Maillard, SONACA
12.20 Composite car-body design of the concept-car C-Metisse using SAMCEF
Emmanuel Lafaury, PSA
12.40 Lunch
14.00 Dynamics of multi-stage cyclic structures
Denis Laxalde, SNECMA (SAFRAN Group)
14.20 Calcul à la fatigue par la méthode des Eléments Finis des réparations des poulies de l’ascenseur à bateaux de Strépy-Thieu
Donatienne Portugaels, MET
14.40 Utilisation des Eléments Finis pour l’étude du comportement d’un mobile-home
Jean-Charles Craveur, ISMANS
15.00 A simple and practical tool to estimate local stress error
Eric Florentin, LMT-Cachan
15.20 Aspect expérimental et contribution à la modélisation des chocs lents
Laurent Beaud, SAINT-GOBAIN Canalisations
15.40 Use of SAMCEF Gateway for the breadboard design of the innovative four mirror anastigmatic telescope with large of view
Jean-Marc Schumacher, AMOS
16.00 Break
16.20 Analysis of inflatable space structures using SAMCEF
Philippe Jetteur, SAMTECH - Stéphane Langlois, ESA
16.40 Comparison of SAMCEF and hierarchical technique for radiative heat transfer
Pierre Beckers, UNIVERSITE DE LIEGE
17.00 High frequency dynamic response computation with SAMCEF Mecano
Alban Du Tertre, SNECMA (SAFRAN Group)
17.20 VEGA electronic boxes vibration analysis
Alain Dumont, SABCA
17.40 Finite Element Analysis using OOFELIE: piezo-thermo-elastic simulations for vibrating inertial sensors
Steve Masson, ONERA
18.00 Closure