Investigation of wing characteristics at a Mach number of 1.53 II : swept wings of taper ratio 0.5

Vincenti, Walter G Van Dyke, Milton D Matteson, Frederick H
naca-rm-a8e05
June 28, 1948


Measured values of lift, drag, and pitching moment at M(sub o) = 1.53 are presented for seven wings varying in sweep angle from 60 degrees sweepforward to 60 degrees sweepback. All wings had a cambered, double-wedge section 5-percent thick and a common taper ratio of 0.5. The experimental results are compared with the predictions of the linear theory.

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