How to Calculate Component of downstream Mach number normal to oblique shock for given normal upstream Mach number?
Component of downstream Mach number normal to oblique shock for given normal upstream Mach number calculator uses Downstream Mach Normal to Oblique Shock = sqrt((1+0.5*((Specific Heat Ratio Dynamic-1)*Component of upstream mach normal to oblique shock^2))/(Specific Heat Ratio Dynamic*Component of upstream mach normal to oblique shock^2-0.5*(Specific Heat Ratio Dynamic-1))) to calculate the Downstream Mach Normal to Oblique Shock, The Component of downstream Mach number normal to oblique shock for given normal upstream Mach number formula is a function of the ratio of specific heat & normal component of upstream Mach no. Downstream Mach Normal to Oblique Shock is denoted by M_{n2} symbol.
How to calculate Component of downstream Mach number normal to oblique shock for given normal upstream Mach number using this online calculator? To use this online calculator for Component of downstream Mach number normal to oblique shock for given normal upstream Mach number, enter Specific Heat Ratio Dynamic (κ) & Component of upstream mach normal to oblique shock (M_{n1}) and hit the calculate button. Here is how the Component of downstream Mach number normal to oblique shock for given normal upstream Mach number calculation can be explained with given input values -> 0.576377 = sqrt((1+0.5*((1.392758-1)*2^2))/(1.392758*2^2-0.5*(1.392758-1))).