from which it was derived, will arrive cut-out patterned in plan form directly after the at an approximately true span load distribution curve upper wing of the Vought Corsair, model 03U-1. with its correlated downwash distribution. In the (See figs. 1 and 2.) The chords of the profiles along… … c Figure 1.—Cut-out wing model. CL — The integration of this expression across the which was faired to an N.A.C.A. 0015 profile at the span can be performed graphically except for the re- center line for considerations of strength. As the gion within some small distance A to either side of the…
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