Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds : body of revolution

John C. Heitmeyer
naca-rm-a51h22
Oct 1951


The lift, drag, and pitching moment of a body of revolution are presented for Mach numbers from 0.60 to 0.92 and from 1.20 to 1.70. These data were obtained at test Reynolds numbers of 0.64 million, 1.02 million, and 1.59 million.

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