NACA research memorandum RM (series). L54C22. Free-flight tests of 45° swept wings of aspect ratio 3.15 and taper ratio 0.54 to measure wing damping of first bending mode and to investigate possibility of flutter at transonic speeds [with list of references]; by Burke R. O'Kelly, Reginald R. Lundstrom, and William T. Lauten, jr.

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