Effectiveness of ailerons in producing roll was measured at various air speeds with full span plain flaps both neutral and deflected 45°; direction of yawing moment created by ailerons is noted.
Flight tests of retractable ailerons on highly tapered wing
Nat Advisory Committee Aeronautics -- Tech Note
1939
9 pages
7 Supp sheets, Bibliography
Report
Englisch
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Flight tests of retractable ailerons on a highly tapered wing
TIBKAT | 1940
|Engineering Index Backfile | 1938
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