How to Calculate Effective Exhaust Velocity of Rocket?
Effective Exhaust Velocity of Rocket calculator uses Effective Exhaust Velocity = Jet Velocity+(Nozzle Exit Pressure-Atmospheric Pressure)*Exit Area/Propellant Mass Flow Rate to calculate the Effective Exhaust Velocity, The Effective Exhaust Velocity of Rocket is the velocity of an exhaust stream after reduction by effects such as friction, non-axially directed flow, and pressure differences between the inside of the rocket and its surroundings. Effective Exhaust Velocity is denoted by c symbol.
How to calculate Effective Exhaust Velocity of Rocket using this online calculator? To use this online calculator for Effective Exhaust Velocity of Rocket, enter Jet Velocity (V_{e}), Nozzle Exit Pressure (p_{2}), Atmospheric Pressure (p_{3}), Exit Area (A_{2}) & Propellant Mass Flow Rate (ṁ) and hit the calculate button. Here is how the Effective Exhaust Velocity of Rocket calculation can be explained with given input values -> 178187.6 = 2151.8+(1240000-101300)*1.75/11.32.