04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
SOME EXPERIMENTAL RESULTS ON DYNAMIC AEROELASTICITY OF PLATES AND SHELLS IN SUBSONIC AND SUPERSONIC FLOW.
J. Lübker, Germany
This paper presents experimental wind tunnel activities on the aeroelastic stability of rectangular and flat plates in low supersonic and high subsonic flow. By means of pressure and deformation measurement, the Generalized Aerodynamic forces are determined, which give information about the test structures stability.