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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 10

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 10 — liI.A.C.A. Icchziical Mcmpraadum 17o.678 Pig. 1 … A, weight 33, daciper P, "base E, hot-wire anemometer Z, almtter vanes Mtmodel O, oscillograph Q, piezo cpiartz E, aniplifying tube S, support Pig, 1 Arrangement of apparatus.

NASA Technical Reports Server (NTRS)

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

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