Elements of the Wing Section Theory and of the Wing Theory (1925)
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the longitudinal velocity ■2 3 IT Z — Z0 V 1 —2 Or, interchanging symbols, writing z for z0 and vice versa f+1 I wfe /J-s2 (19) For a point near the edge on the positive side, write z0 = l — e -2 or, substituting -yj2e=sm 5edl Tiffin J^^Vrii (19a) For the discussion of the elements of the wing… … Fig. 3.—Circulation flow around a straight line. form any mechanical work, as the transverse components of velocity at points along the line are zero. Tbe kinetic energy of this flow, on the other hand, is infinite, and hence this flow can not even be completely realized. Still it plays the most…
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