Elements of the Wing Section Theory and of the Wing Theory (1925)
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elocity at right angles to dF the real axis is equal to the reversed imaginary part of The absolute magnitude of the ve- dF locity is equal to the absolute magnitude of -g-• 3. I proceed now to the series of two-dimensional flows which are of chief importance for the solution of the aerodynamic… … F=i{z--%fzT=T) (2) Fig 1.—Transverse flow, produced by a moving straight line. represents the fiow.produced by the straight line extending between the points z= ±1, moving transversely in the direction of the negative imaginary axis with the velocity 1 in the fluid other- wise at rest. For its…
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