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Tests of 16 related airfoils at high speed (1935)

NASA Technical Reports Server (NTRS) · leaf 15

An illustration from Tests of 16 related airfoils at high speed, 1935, leaf 15
354 REPORT NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS … Fiodhe 35.—Effect of compressibility on profile drag. .24r .24 .20 .20 .16 .16 dCj. del del .12 .12 .08 .08 .04 .04 .6 .8 1.0 1.2 .4 1.2 I.O .8 .6 V/Vc V/Vc on llftcarve slope. Variation with position Fiocbe 38.—Effect of compressmDUty on lift-curve slope. Variation with thickness. Fiquee…

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