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The flight of an autogiro at high speed (1933)
NASA Technical Reports Server (NTRS) · leaf 17
1T.A.C.A. Technical Memorandum 17o. 729 Figs. 5,6 .20 30 l-cvnn = .0)20 .40 1.00 .15 n! .70 50 / .(10 .012 i i >7 ,„ X -i—r i ' .004 .05 -i •- / cwm - 0 i i i .10 .02 .08 .04 .06 "a Figure 5.- Effect of profile drag on W/A a, = .07 = .*o <T = .07; … Figure 6.- Sffoct of solidity on W/A a, = 4° - .07; cv/m = .012; i = 9.76NASA Technical Reports Server (NTRS)
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