How to Calculate Stagnation Pressure behind Normal Shock by Rayleigh Pitot Tube formula?
Stagnation Pressure behind Normal Shock by Rayleigh Pitot Tube formula calculator uses Stagnation Pressure Behind Normal Shock = Static Pressure Ahead of Normal Shock*((1-Specific Heat Ratio+2*Specific Heat Ratio*Mach Number Ahead of Normal Shock^2)/(Specific Heat Ratio+1))*(((Specific Heat Ratio+1)^2*Mach Number Ahead of Normal Shock^2)/(4*Specific Heat Ratio*Mach Number Ahead of Normal Shock^2-2*(Specific Heat Ratio-1)))^((Specific Heat Ratio)/(Specific Heat Ratio-1)) to calculate the Stagnation Pressure Behind Normal Shock, The Stagnation Pressure behind Normal Shock by Rayleigh Pitot Tube formula calculates the stagnation pressure of a fluid behind a normal shock wave using the Rayleigh Pitot Tube formula. This equation incorporates parameters such as the static pressure ahead of the shock, the Mach number ahead of the shock, and the ratio of specific heats for the fluid. It provides valuable insights into the change in stagnation pressure as the fluid passes through the shock wave, aiding in the analysis of compressible flow phenomena. Stagnation Pressure Behind Normal Shock is denoted by p02 symbol.
How to calculate Stagnation Pressure behind Normal Shock by Rayleigh Pitot Tube formula using this online calculator? To use this online calculator for Stagnation Pressure behind Normal Shock by Rayleigh Pitot Tube formula, enter Static Pressure Ahead of Normal Shock (P1), Specific Heat Ratio (γ) & Mach Number Ahead of Normal Shock (M1) and hit the calculate button. Here is how the Stagnation Pressure behind Normal Shock by Rayleigh Pitot Tube formula calculation can be explained with given input values -> 220.6775 = 65.374*((1-1.4+2*1.4*1.49^2)/(1.4+1))*(((1.4+1)^2*1.49^2)/(4*1.4*1.49^2-2*(1.4-1)))^((1.4)/(1.4-1)).