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The aerodynamic characteristics of six commonly used Airfoils over a large range of positive and negative angles of attack (1931)

NASA Technical Reports Server (NTRS) · leaf 11

An illustration from The aerodynamic characteristics of six commonly used Airfoils over a large range of positive and negative angles of attack, 1931, leaf 11 — * … -?& -24° -16° -8° 0° 8° 16° 24° 32° Angle of attack, <x 3?ig. 6 Airfoil, Gbtt. 398. Reynold's BFumber, 3,100,000. V.D.T. tests, hg4 said 639. Aspect ratio, 6, Dates s/31 and 7/33.. Tunnel wall correction applied. i

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