Experimental and theoretical studies of panel flutter at Mach numbers 1.2 to 3.0
1955-07-19
Miscellaneous
No indication
English
Theoretical considerations of panel flutter at high supersonic Mach numbers
Engineering Index Backfile | 1966
|Theoretical and experimental panel flutter studies in mach number range 1.0 to 5.0
Engineering Index Backfile | 1965
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