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Tests for determining the effect of a rotating cylinder fitted into the leading edge of an airplane wing (1926)

NASA Technical Reports Server (NTRS) · leaf 18

An illustration from Tests for determining the effect of a rotating cylinder fitted into the leading edge of an airplane wing, 1926, leaf 18 — u <D <d … tJ O o CD £-4 1 I t I 1 } i <J X + O } ! f I I I o I i

NASA Technical Reports Server (NTRS)

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

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