First experimental Investigations on DynamicAeroelastic Stability of Panels in the TransonicDomain at the German Aerospace Center (DLR)
2017
An forced motion experiment on earoelastic stability is performed within a Mach number
domain of 0:7 < M < 1:2. The panel structure is de
ected in its first bending mode shape.
The objective is to obtain the aerodynamic response over an extensive range of amplitudes
and frequencies of panel motions. Beside the measurement of the panel deformation by
a stereo camera marker tracking system, the
ow response is measured by high sensitive
miniature pressure transducers. Results of pressure coefficient distribution measurements
and deformation measurements are presented. Concluding, first preliminary comparisons
of experimental data and numerical results gained within the project are are discussed.
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