Models having aspect ratios ranging from 2 to 13 were tested at Mach numbers up to 0.92; examination of data is made on basis of reference theoretical values obtained from 2-dimensional incompressible flow theory; on this basis reduction in aspect ratio increased ratio of experimental to calculated flutter speed.
Experimental investigation of effect of aspect ratio and Mach number on flutter of cantilever wings
NASA -- Tech Note
1960
20 pages
Report
Englisch
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Initial experiments on flutter of unswept cantilever wings at mach number 1.3
Engineering Index Backfile | 1954
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