How to Calculate Throat Velocity of Nozzle?
Throat Velocity of Nozzle calculator uses Throat Velocity = sqrt((2*Specific Heat Ratio)/(Specific Heat Ratio+1)*[R]*Temperature at Chamber) to calculate the Throat Velocity, The Throat Velocity of Nozzle refers to the velocity of the exhaust gases as they pass through the narrowest section of the rocket engine nozzle, it is a crucial parameter in rocket engine design as it determines the maximum velocity of the exhaust gases at the throat. Throat Velocity is denoted by v_{t} symbol.
How to calculate Throat Velocity of Nozzle using this online calculator? To use this online calculator for Throat Velocity of Nozzle, enter Specific Heat Ratio (γ) & Temperature at Chamber (T_{1}) and hit the calculate button. Here is how the Throat Velocity of Nozzle calculation can be explained with given input values -> 49.29467 = sqrt((2*1.33)/(1.33+1)*[R]*256).