ANALYSIS OF THE STATIC AND DYNAMIC AERO-STRUCTURAL RESPONSE OF AN ELASTIC SWEPT WING MODEL BY DIRECT AEROELASTIC SIMULATION

摘要

In this report the numerical method SOFIA for direct aeroelastic simulation is applied to a sweptwing wind tunnel configuration in the subsonicflow regime. The computational results reveal agood aggreement of the deformations and clamp-ing reactions predicted by SOFIA with the per-formed wind tunnel results. This is valid for theaeroelastic equilibrium configuration as well asfor the dynamic response tests.