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A flight and wind tunnel investigation of the effect of angle-of-attack rate on maximum lift coefficient

Conner, F.
Twomey, W.
Willey, C.

Publication date

October 1965

Language

English

Abstract

Wind tunnel tests to determine effect of angle of attack on maximum lift at stall for half-wing models, and single engine, jet propelled aircraf

Extracted data

Topics

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Wind tunnelSoftware

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