How to Calculate Temperature behind oblique shock for given upstream temperature and normal upstream Mach number?
Temperature behind oblique shock for given upstream temperature and normal upstream Mach number calculator uses Temperature behind Shock = Temperature ahead of Shock*((1+((2*Specific Heat Ratio Dynamic)/(Specific Heat Ratio Dynamic+1))*((Component of upstream mach normal to oblique shock^2)-1))/((Specific Heat Ratio Dynamic+1)*(Component of upstream mach normal to oblique shock^2)/(2+((Specific Heat Ratio Dynamic-1)*(Component of upstream mach normal to oblique shock^2))))) to calculate the Temperature behind Shock, The Temperature behind oblique shock for given upstream temperature and normal upstream Mach number formula is obtained by multiplying the temperature ahead of an oblique shock to temperature ratio across the oblique shock. Temperature behind Shock is denoted by T_{s2} symbol.
How to calculate Temperature behind oblique shock for given upstream temperature and normal upstream Mach number using this online calculator? To use this online calculator for Temperature behind oblique shock for given upstream temperature and normal upstream Mach number, enter Temperature ahead of Shock (T_{s1}), Specific Heat Ratio Dynamic (κ) & Component of upstream mach normal to oblique shock (M_{n1}) and hit the calculate button. Here is how the Temperature behind oblique shock for given upstream temperature and normal upstream Mach number calculation can be explained with given input values -> 2380.489 = 789*((1+((2*1.392758)/(1.392758+1))*((2^2)-1))/((1.392758+1)*(2^2)/(2+((1.392758-1)*(2^2))))).