Aeroelastic stability of cylindrical shells subjected to a rotating flow
12th Aerospace Sciences Meeting ; 1974 ; Washington , DC , U.S.A.
01.01.1974
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
AEROELASTIC STABILITY OF CYLINDRICAL SHELLS IN SUPERSONIC FLOW WITH BOUNDARY LAYER (AIAA 2017-3618)
British Library Conference Proceedings | 2017
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