How to Calculate Pressure behind oblique shock for given upstream pressure and normal upstream Mach number?
Pressure behind oblique shock for given upstream pressure and normal upstream Mach number calculator uses Static pressure behind shock = Static pressure ahead of shock*(1+((2*Specific Heat Ratio Dynamic)/(Specific Heat Ratio Dynamic+1))*((Component of upstream mach normal to oblique shock^2)-1)) to calculate the Static pressure behind shock, The Pressure behind oblique shock for given upstream pressure and normal upstream Mach number formula is obtained by multiplying the pressure ahead of an oblique shock to pressure ratio across the oblique shock. Static pressure behind shock is denoted by P_{b} symbol.
How to calculate Pressure behind oblique shock for given upstream pressure and normal upstream Mach number using this online calculator? To use this online calculator for Pressure behind oblique shock for given upstream pressure and normal upstream Mach number, enter Static pressure ahead of shock (P_{a}), Specific Heat Ratio Dynamic (κ) & Component of upstream mach normal to oblique shock (M_{n1}) and hit the calculate button. Here is how the Pressure behind oblique shock for given upstream pressure and normal upstream Mach number calculation can be explained with given input values -> 71.87893 = 16*(1+((2*1.392758)/(1.392758+1))*((2^2)-1)).