Experiments were performed with a wing model, to which a rotary cylinder had been fitted. The rotation of the cylinder had a remarkable effect on the aerodynamic properties of the wing.
Tests for determining the effect of a rotating cylinder fitted into the leading edge of an airplane wing
International Congress of Aerial Navigation (3rd : 1925 : Brussels)
1926-03-01
Sonstige
Keine Angabe
Englisch
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