Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds : plane 45 degree swept-back wing of aspect ratio 3, taper ratio 0.4 with 3-percent- thick, biconvex section

John C. Heitmeyer
naca-rm-a51h10
Sep 1951


A wing-body combination having a plane 45 degree swept-back wing of aspect ratio 3, taper ratio 0.4, and 3-percent-thick biconvex sections in streamwise planes has been investigated at both subsonic and supersonic Mach numbers. The lift, drag, and pitching moment of the model are presented for Mach numbers from 0.60 to 0.92 and from 1.20 to 1.70 at a Reynolds number of 3.83 million.

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