Effect of leading-edge sweepback on lift, drag, and pitching-moment characteristics of thin wings of aspect ratio 3 and taper ratio 0.4 at subsonic and supersonic speeds

Wetzel, Benton E.
naca-rm-a55h04a
1955


Results indicating the effect of leading-edge sweep-back on the lift, drag, and pitching moment are presented for wings of aspect ratio 3 and taper ratio 0.4 with thickness-chord ratio 0.03.

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