How to Calculate Static Temperature behind Normal Shock for given Upstream Temperature and Mach Number?
Static Temperature behind Normal Shock for given Upstream Temperature and Mach Number calculator uses Temperature Behind Normal Shock = Temperature Ahead of Normal Shock*((1+((2*Specific Heat Ratio)/(Specific Heat Ratio+1))*(Mach Number Ahead of Normal Shock^2-1))/((Specific Heat Ratio+1)*(Mach Number Ahead of Normal Shock^2)/(2+(Specific Heat Ratio-1)*Mach Number Ahead of Normal Shock^2))) to calculate the Temperature Behind Normal Shock, Static Temperature behind Normal Shock for given Upstream Temperature and Mach Number formula is defined as a method to determine the temperature of a gas after it passes through a normal shock wave, considering the upstream conditions and Mach number. Temperature Behind Normal Shock is denoted by T2 symbol.
How to calculate Static Temperature behind Normal Shock for given Upstream Temperature and Mach Number using this online calculator? To use this online calculator for Static Temperature behind Normal Shock for given Upstream Temperature and Mach Number, enter Temperature Ahead of Normal Shock (T1), Specific Heat Ratio (γ) & Mach Number Ahead of Normal Shock (M1) and hit the calculate button. Here is how the Static Temperature behind Normal Shock for given Upstream Temperature and Mach Number calculation can be explained with given input values -> 391.6411 = 298.15*((1+((2*1.4)/(1.4+1))*(1.49^2-1))/((1.4+1)*(1.49^2)/(2+(1.4-1)*1.49^2))).