General formulation of 3-dimensional flow problem with application to calculation of wall interference in wind tunnel testing at high speeds is given; wing theory is examined from usual point of view; this involves derivation of Biot-Savart law for compressible flow by Glauert-Prandtl approximation. (See also - discussion in n 4 Oct p 432)
Glauert-Prandtl approximation for subsonic flows of compressible fluid
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 12 , n 4
1945
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