Investigation included determination of rolling and yawing characteristics of airplane in abrupt aileron rolls with slotted flap at various settings ranging from 0° to 40°; effectiveness of ailerons greatly reduced at flap deflections greater than 20°.
Flight measurements of lateral control characteristics of narrow-chord ailerons on trailing edge of full-span slotted flap
Nat Advisory Committee Aeronautics -- Tech Note
1947
6 pages
13 Supp Plates
Report
Englisch
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Engineering Index Backfile | 1947
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