Flutter investigation in the transonic range of six airfoils attached to three freely falling bodies

S. A. Clevenson, William T. Lauten, Jr.
naca-rm-l7k17
May 1948


Results of tests of six flutter wings, two swept 45 degrees and four unswept, attached to three freely falling bodies are reported. Two unswept wings fluttered at transonic Mach numbers of 0.840 and 0.895, and two similar wings with 45 degrees sweepback fluttered at 0.920 and 0.925.

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