Preliminary tests on model of monoplane wing equipped with wing-tip floating ailerons; lift, drag, and rolling and yawing moments found; rolling moments roughly independent of angle of attack and yawing moments small; with ailerons neutral minimum drag was more than twice that of wing without ailerons; more suitable plan forms and profiles for wing and ailerons would give improved results.
Wind tunnel tests on a model of a monoplane wing with floating ailerons
Nat. Advisory Committee Aeronautics -- Tech. Note
1929
13 pages
10 Figs. on supp. plates, Bibliography
Report
Englisch
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The effect of wing tip floating ailerons on the autorotation of a monoplane wing model
Engineering Index Backfile | 1930
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