Rolling and yawing moments due to ailerons of various chords and spans on Clark-Y and U.S.A.-27 wing sections studied; effect of scale on rolling and yawing moments; effect of slightly rounding wing tips; results apply to level flight with wing chord set at plus 4-deg. angle of attack and to zero pitch, yaw, and roll; work conducted in 10-ft. Bureau of Standards wind tunnel.
Effect of variation of chord and span of Ailerons on rolling and yawing moments in level flight
Nat. Advisory Committee Aeronautics -- Report
1929
19 pages
27 Figs., Bibliography
Report
Englisch
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Engineering Index Backfile | 1931
|Rolling, yawing, and hinge moments produced by rectangular ailerons
Engineering Index Backfile | 1933
|