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Increase in the maximum lift of an airplane wing due to a sudden increase in its effective angle of attack resulting from a gust (1932)

NASA Technical Reports Server (NTRS) · leaf 11

An illustration from Increase in the maximum lift of an airplane wing due to a sudden increase in its effective angle of attack resulting from a gust, 1932, leaf 11 — H.A.C.A. Technical Memoraadam Ho. 678 JlgBm 2,3

NASA Technical Reports Server (NTRS)

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

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