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Wind tunnel force tests in wing systems through large angles of attack (1928)

NASA Technical Reports Server (NTRS) · leaf 10

An illustration from Wind tunnel force tests in wing systems through large angles of attack, 1928, leaf 10 — N.A.C.A. Technical Note No.294 Fig.3 0 .2 .4 .6 GD .8 1.0 1.2 1.4 Fig.3 Monoplane wings,tip shape effect.

NASA Technical Reports Server (NTRS)

Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.

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