Wind-tunnel research comparing lateral control devices, particularly at high angles of attack I : ordinary ailerons on rectangular wings (1933)
NASA Technical Reports Server (NTRS) · leaf 6
363 ORDINARY AILERONS ON RECTANGULAR "WINGS .060 .too Right aileron 0' _ Left aileron down + 10° O 20' .040 .030 Q 30' — A 40' ■o 020 .060 JS- cy 3 .040\ _ — S -.020 .020ki Fiotoe 8.—Honing and yawing moment coefficients doe to 28 per cent chord aileron down. Ailerons looked; —20° yaw -.020 40'… … Piques 10.—Boiling and yawing moment coefficients due to 25 per cent Figure 11.—Rolling and yawing moment coefficients due to 26 per cent chord ailerons up and down. Ailerons floating; 0° yaw chord anerons up and down. .Ailerons floating; —20° yaw
NASA Technical Reports Server (NTRS)
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