Characteristics of ailerons in Reports nos. 298, 343 and 370 summarized in form of empirical equations which relate aileron dimensions and displacements to rolling, yawing, and hinge moments for pitch angles of 0 and 12°, corresponding to angles of attack of wings of 4 and 16°.
Rolling, yawing, and hinge moments produced by rectangular ailerons
Nat Advisory Committee Aeronautics -- Tech Notes
1933
12 pages
3 Supp Sheets
Aufsatz (Zeitschrift)
Englisch
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Engineering Index Backfile | 1934
|Effect of variation of chord and span of Ailerons on rolling and yawing moments in level flight
Engineering Index Backfile | 1929
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