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Total flow conditions or stagnation upstream of the normal shock conditions that we would get if we could slow the throat "corner".
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Normal Shock Waves � Lesson 2A useful little tool for calculating the properties across a normal shock. Normal Shock Calculations Input a freestream Mach number and ratio of specific heats. Compute compressible aerodynamics properties using isentropic, normal shock, or oblique shock relations. This calculator is an aid in making calculations in compressible fluid dynamics, such as isentropic flow, normal shock, oblique shock, Rayleigh and Fanno flow.
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