Pressure Distribution Tests on PW-9 Wing Models from -18 Degree Through 90 Degree Angle of Attack (1929)
NASA Technical Reports Server (NTRS) · leaf 6
5 PRESSURE DISTRIBUTION TESTS ON PW-9 WING MODELS … Fk;. 2.—Plan and front elevation of PW-y wing models. Oottingen 436 airfoil Pressure survey Pressure head, cm a/cohol. Pifof-staiic tube O - 5"Angle ofaHack P'iG. 3.—Longitudinal section of wind tunnel
NASA Technical Reports Server (NTRS)
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