Effects of a series of inboard plan-form modifications on the longitudinal characteristics of two 47 degree sweptback wings of aspect ratio 3.5, taper ratio 0.2, and different thickness distributions at Mach numbers of 1.61 and 2.01

Cooper, Morton Sevier, John R , Jr
naca-rm-l53e07a
July 17, 1953


No Abstract Available

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