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Results of Two Free-fall Experiments on Flutter of Thin Unswept Wings in the Transonic Speed Range

WIlliam T. Lauten

出版	National Advisory Committee for Aeronautics, 1951
URL	http://books.google.com.hk/books?id=uj0PSbH6ixIC&hl=&source=gbs_api
EBook	FULL_PUBLIC_DOMAIN

註釋

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 Mach number of 1.0, are presented.