The present paper deals with steady and unsteady aeroelastic simulation results obtained on the High Reynolds Number Aero-Structural Dynamics (HIRENASD) wind tunnel configuration [1], selected as common test case in the numerical aeroelasticity ONERA/DLR cooperation project “NLAS2”. In order to assess the aeroelastic prediction capabilities of the flow solvers elsA (ONERA) and TAU (DLR), 3 types of simulations have been realized: static coupling, harmonic forced motion and dynamic coupling. The set-up of the numerical simulations as well as comparisons with experimental data are presented for selected test cases.
Assessment of the ONERA/DLR numerical aeroelastics prediction capabilities on the HIRENASD configuration
2011 ; Paris, Frankreich
2011
Conference paper
Electronic Resource
German
numerical , deflection , aerodynamics , structural mode , experimental , loads , damping , twist , frequency , aeroelasticity , High Re , wing-body , external flow
IEEE | 2011
|British Library Conference Proceedings | 2016
|