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- W825390562 abstract "The results of some wind-tunnel experiments to investigate the effects of aspect ratio and Mach number on the flutter of uniform, unswept, cantilever wings are reported. Models having aspect ratios ranging from 2 to 13 were tested at Mach numbers up to 0.92. No general attempt is made to correlate the data with three-dimensional-flow theory, but an examination of the data is made on the basis of reference theoretical values obtained from the two-dimensional incompressible-flow theory. On this basis a reduction in aspect ratio, in general, increased the ratio of the experimental flutter speed to the calculated flutter speed. The analysis also indicated that for a given aspect ratio, this ratio decreased slightly as the Mach number is increased." @default.
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- W825390562 date "1950-06-01" @default.
- W825390562 modified "2023-09-27" @default.
- W825390562 title "Experimental investigation of the effect of aspect ratio and Mach number on the flutter of cantilever wings" @default.
- W825390562 hasPublicationYear "1950" @default.
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