Comparative Flight and Full-Scale Wind-Tunnel Measurements of the Maximum Lift of an Airplane (1938)
NASA Technical Reports Server (NTRS) · leaf 4
corre- Determinations of the power-off maximum lift of a sponding to two airplane loadings used in the Might tests. Fair child 22 airplane were made in the N. A. C. A. full- The airplane was equipped for these tests with a scale wind tunnel and in flight. The results from, the specially surfaced… … Figure 1.—Fairchild 22 airplane with wing of N. A. C. A. 2Ril2 section. Wind-tunnel tests to determine the Reynolds Num- ber effects on the maximum lift coefficient and on the of the wing surface and waxed to a reflecting finish, the minimum drag coefficient were also made. polish being maintained…
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