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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 16

An illustration from Tests for determining the effect of a rotating cylinder fitted into the leading edge of an airplane wing, 1926, leaf 16 — • Pi H p> CX2 -P O H 03 O a) fH CO H 0.) oD w > -H … O •H t! ii 0) O Eh o

NASA Technical Reports Server (NTRS)

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

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