Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds : plane tapered wing of aspect ratio 3.1 with 3-percent-thick, biconvex section

David E. Reese, E. Ray Phelps
naca-rm-a50k28
Jan 1951


A wing-body combination having a plane tapered wing of aspect ratio 3.1 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 0.925 and 1.20 to 1.90 at a Reynolds number of 2.4 million.

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