Effect of Variation of Chord and Span of Ailerons on Rolling and Yawing Moments in Level Flight (1929)
NASA Technical Reports Server (NTRS) · leaf 11
10 REPORT NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS … .24 . , , I I I I I 1 1 I I I O Aileron spon 20in. ■\-Aileron spon 20 in ' I I chord 3.0 I I chord 3.5 '•. -6 Up oiler on • Do wn oileron - % Aileron spon 20 '. X Aileron spon 20 ". .20 ■ I I c/7ord 2.5" chord 2.0 Q Aileron spon 20 " 44' — ctiord 1.5 " .16 ^24' .12 .06 16' .04 24' 32' 16' 24" 32"…
NASA Technical Reports Server (NTRS)
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