Report no. 344. The design of plywood we
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Article
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1930
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Elsevier Science
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English
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The measurements were made at various angles of pitch but at zero angle of roll and yaw, the wing chord being set at an angle of + 4 ยฐ to, the fuselage axis. In the case of the Clark Y airfoil the measurements have been extended to a pitch angle of 4 oยฐ, using ailerons of span equal to 67 per cent.