Effect of Structural Parameters on Shock Wave Boundary Layer Induced Panel Flutter
AIAA Aviation 2019 Forum
2019-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
AIAA-2019-3716: Effect of Structural Parameters on Shock Wave Boundary Layer Induced Panel Flutter
British Library Conference Proceedings | 2019
|Boundary-layer effect in panel flutter
NTRS | 1975
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