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Theory of wing sections of arbitrary shape (1933)

NASA Technical Reports Server (NTRS) · leaf 11

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noted that a is measured from the line of y-e* ■(f)" sin Q-e* 2a sinh f Vsinh2 l/' + sin2 6 I . ,, , , / y VSmh'K2asinh*. and ■ay ,2* (2a2/)2 P. (2a smb. </-)*+(2 cn/)2 i This result checks exactly with the form given by Dr. A. F. Zahm in N. A. C. A. Technical Report No. Figure 6.—Clark Y… … Figuee 7.—The unit circle 2=e'*, the circle z=e*rfi*, and the corresponding (See figs. 7 and 8). Column 12 gives the quantity curve z'—e" Upper si .-fjee e Fiouse 8—(a) T„e & against 6 curve for the Clark Y. (6) The t against B curve for the Clark ^

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