Theoretical and experimental panel flutter studies in the Mach number range 1.0 to 5.0
1st Annual Meeting ; 1964 ; Washington , DC , U.S.A.
1964-01-01
Conference paper
Electronic Resource
English
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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