AIAA-2019-3716: Effect of Structural Parameters on Shock Wave Boundary Layer Induced Panel Flutter
Fluid dynamics ; 2019 ; Dallas, TX
01.01.2019
24 pages
Aufsatz (Konferenz)
Englisch
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Panel Flutter Induced by Transitional Shock Wave Boundary Layer Interaction (AIAA 2018-3548)
British Library Conference Proceedings | 2018
|DataCite | 1916