3/7/13    14:00 - 17:20
MS.5: Loads and Aeroelasticity
WeA08
Room: Novotel Chiemsee
Chair: Jean-Pierre Grisval
CoChair: Wolfgang Lüber
Rapporteur: to be confirmed
High and low fidelity finite element modelling in aircraft composite fuselage structural analysis and optimisation
WJ Vankan, BAT Noordman and K Kueres


Elastic body impact on sandwich panels at low and intermediate velocity(*)
C. Kralovec, M. Schagerl and K.U. Schröder


On the use of lyophobic heterogeneous systems (LHS) in payload comfort(*)
M. Michelin-Jamois, L. Guillemot, T. Abensur, E. Charlaix and G. Vigier


Aeroelastic tailoring of a blended wing body (BWB) aircraft structure using FSI simulation
F. Stroscher, A. Hermanutz, N. Maghaldadze and H. Baier


Stand with artificial airflow simulation and flutter tests results of dynamically scaled model
V.I. Smyslov, M.M. Bogatyrev, P.G. Karlke and G.V. Liseykin


Aeroelastic Rotor Blade Dynamics for Helicopter Flight Mechanics Applications
I. Goulos, V. Pachidis and P. Pilidis


Fuselage damping characteristics and fatigue blade impact on the stability of helicopter (*)
A. Nour, S. Lecheb, A. Chellil and H. Kebir