How to Calculate Exit Velocity given Mach number and Exit Temperature?
Exit Velocity given Mach number and Exit Temperature calculator uses Exit velocity = Mach Number*(Specific Heat Ratio*Universal Gas Constant*Exit Temperature)^0.5 to calculate the Exit velocity, Exit Velocity given Mach number and Exit Temperature formula is used to determine the velocity that is produced at the end of the rocket's nozzle or exhaust if we know the Mach number and the exit temperature. Exit velocity is denoted by c_{2} symbol.
How to calculate Exit Velocity given Mach number and Exit Temperature using this online calculator? To use this online calculator for Exit Velocity given Mach number and Exit Temperature, enter Mach Number (M), Specific Heat Ratio (k), Universal Gas Constant (R) & Exit Temperature (T_{exit}) and hit the calculate button. Here is how the Exit Velocity given Mach number and Exit Temperature calculation can be explained with given input values -> 151.6131 = 8*(1.6*8.314*27)^0.5.