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 … Rouse 9.—Boiling and yawing moment coefficients due to 25 per cant chord aileron np. Ailerons looked; —20° yaw 3 o -.oeo}- :04O 20° 30- IO° 40- 4C° a 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…
NASA Technical Reports Server (NTRS)
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