Aeroelastic stability of cylindrical shells subjected to a rotating flow
12th Aerospace Sciences Meeting ; 1974 ; Washington , DC , U.S.A.
1974-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Aeroelastic Stability Characteristics of Composite Cylindrical Shells by the Finite Element Method
British Library Online Contents | 1992
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