An experimental investigation of the flutter of several wings of varying aspect ratio, density, and thickness ratio at Mach numbers from 0.60 to 1.10
1954-04-07
Miscellaneous
No indication
English
Experimental investigation of effect of aspect ratio and Mach number on flutter of cantilever wings
Engineering Index Backfile | 1960
|Characteristics of low-aspect-ratio wings at supercritical mach numbers
Engineering Index Backfile | 1950
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