Ratio of Stagnation and Static Pressure evaluator uses Stagnation to Static Pressure = (1+((Specific Heat Ratio-1)/2)*Mach Number^2)^(Specific Heat Ratio/(Specific Heat Ratio-1)) to evaluate the Stagnation to Static Pressure, Ratio of Stagnation and Static Pressure formula is defined as a relationship that describes the pressure differences in a compressible flow, illustrating how stagnation pressure relates to static pressure in various aerodynamic conditions. Stagnation to Static Pressure is denoted by Pr symbol.
How to evaluate Ratio of Stagnation and Static Pressure using this online evaluator? To use this online evaluator for Ratio of Stagnation and Static Pressure, enter Specific Heat Ratio (γ) & Mach Number (M) and hit the calculate button.