Application of slender body theory to missiles with arbitrary shape cross sections
24th Aerospace Sciences Meeting ; 1986 ; Reno , NV , U.S.A.
1986-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Aeroelastic stability of slender, spinning missiles
AIAA | 1992
|Aeroelastic stability of slender, spinning missiles
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|Application of slender-body theory
Engineering Index Backfile | 1957
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