Charts for determining the characteristics of sharp-nose airfoils in two-dimensional flow at supersonic speeds

Ivey, H Reese Stickle, George W Schuettler, Alberta

Solutions of the Hugoniot shock equations and Meyer expansion equations are plotted in such a manner as to permit the pressure distribution, the local Mach number, and the angles of shock waves on arbitrary sharp-nose airfoils at supersonic speeds to be obtained directly. (author)

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