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Airfoil Theory at Supersonic Speed (1939)

NASA Technical Reports Server (NTRS) · leaf 57

An illustration from Airfoil Theory at Supersonic Speed, 1939, leaf 57
N.A.C.A. Technical Memorandum Ho. 897 Figs. 7,8,9,10 Figure 7.- Bectangular wing as Figure 8.- Rectangular wing as lifting surface with lifting surface with constant lift distribution. constant lift distribution. Streamline picture of the y- and s~ Streamline picture of the y- and z- velocities in… … Figure 10.*- Trapetoidal wing with constant lift distribution. Coefficients of/ISto wave plus induced drag Cw/4tancc as a function of ihi> *re due e4 aspect ratio0 A = t tan<^b for various trapezoid shapes 0 »-taiiT/tanoC.

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