Aeroelastic Coupling Between a Shock-Wave/turbulent Boundary-Layer Interaction and a Flexible Panel
L. Laguarda (TU Delft - Aerospace Engineering)
S. Hickel (TU Delft - Aerospace Engineering)
F. F.J. Schrijer (TU Delft - Aerospace Engineering)
B. W. van Oudheusden (TU Delft - Aerospace Engineering)
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Abstract
Oscillating loads from shock-wave/turbulent boundary-layer interactions (STBLIs) can cause structural components to resonate and potentially fail due to high-cycle fatigue.