Results of four thin, unswept, flutter airfoils attached to two freely falling bodies are reported. Two airfoils fluttered at a Mach number of 0.85, a third airfoil fluttered at a Mach number of 1.03, and a fourth fluttered at a Mach number of 1.07. Results of calculations of flutter speed using incompressible and compressible air-force coefficients, including a Mach number of 1.0, are presented.
Results of Two Free-fall Experiments on Flutter of Thin Unswept Wings in the Transonic Speed Range
01.01.1957
Sonstige
Keine Angabe
Englisch
Initial experiments on flutter of unswept cantilever wings at mach number 1.3
Engineering Index Backfile | 1954
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