This report describes preliminary wind tunnel tests on a model of a monoplane wing equipped with wing tip floating ailerons. Lift and drag, as well as rolling and yawing moments, were measured.
Wind Tunnel Tests on a Model of a Monoplane Wing with Floating Ailerons
01.09.1929
Sonstige
Keine Angabe
Englisch
Wind tunnel tests on a model of a monoplane wing with floating ailerons
Engineering Index Backfile | 1929
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