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 equation, relates the ratio of stagnation pressure to static pressure to the Mach number of the flow and the specific heat ratio of the gas. It demonstrates how the pressure of a compressible flow changes due to the effects of compression or expansion associated with changes in flow velocity and Mach number. 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.