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Pressure Distribution Tests on PW-9 Wing Models from -18 Degree Through 90 Degree Angle of Attack (1929)

NASA Technical Reports Server (NTRS) · leaf 19

An illustration from Pressure Distribution Tests on PW-9 Wing Models from -18 Degree Through 90 Degree Angle of Attack, 1929, leaf 19 — 18 REPORT NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS … Fig. 23.—Semispan loading

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