Theoretical and experimental panel flutter studies in the Mach number range 1.0 to 5.0.
DOWELL, E. H., VOSS, H. M. /BOEING CO., AERO-SPACE DIV., SEATTLE, WASH./.
AIAA Journal ; 3 , 12 ; 2292-2304
1965
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Theoretical and experimental panel flutter studies in mach number range 1.0 to 5.0
Engineering Index Backfile | 1965
|Some experimental studies of panel flutter at Mach number 1.3
TIBKAT | 1957
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