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Tests of 16 related airfoils at high speed (1935)

NASA Technical Reports Server (NTRS) · leaf 9

An illustration from Tests of 16 related airfoils at high speed, 1935, leaf 9
ADVISORY COMMITTEE FOB AERONAUTICS REPORT NATIONAL … of the NA.OA. 2409-34 alrfolL Figdbe 17.—Effect of compressibility on the aerodynamic characteristics .14 Angle of attack >-4" x-2° o 0° +2° a 4" .12 C ■3 m o u 08 5 .J! .06 l_, 0 for 4° .04 .u ■' O for . o O for 0° .02 0 for -2° 6-./ O for -4° 1.0 4 .6 .2 0 O .2 .4 £ .8 .4 .6? .S v/vc v/vc Figure…

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