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Pressure Distribution Over a Rectangular Monoplane Wing Model up to 90 Degree Angle of Attack (1929)

NASA Technical Reports Server (NTRS) · leaf 12

An illustration from Pressure Distribution Over a Rectangular Monoplane Wing Model up to 90 Degree Angle of Attack, 1929, leaf 12
11 PRESSURE DISTRIBUTION OVER A RECTANGULAR MONOPLANE WING MODEL … Figs. 19, 20, and 21.—Resultant normal prcs.^ure distribution

NASA Technical Reports Server (NTRS)

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

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