An approximate method of calculating pressures in the tip region of a rectangular wing of circular-arc section at supersonic speeds

Kazimierz Roman Czarnecki, James N. Mueller
naca-tn-2211
Oct 1950


An approximate method of calculating pressures within the tip region of a rectangular wing having a symmetrical circular-arc profile is developed by means of which it is possible to determine the pressures at supersonic speeds to a higher degree of accuracy than the usual linearized methods.

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