How to Calculate Exhaust Velocity given Gross Thrust in Turbojet?
Exhaust Velocity given Gross Thrust in Turbojet calculator uses Exit Velocity = (Gross Thrust of Turbojet-(Nozzle Exit Pressure-Ambient Pressure)*Nozzle Exit Area)/(Mass Flow Rate Turbojet*(1+Fuel Air Ratio)) to calculate the Exit Velocity, Exhaust Velocity given Gross Thrust in Turbojet is a measure of the velocity at which gases escape the nozzle of a turbojet engine, affecting the engine's performance and efficiency, and is influenced by factors such as gross thrust, atmospheric pressure, and nozzle area. Exit Velocity is denoted by Ve symbol.
How to calculate Exhaust Velocity given Gross Thrust in Turbojet using this online calculator? To use this online calculator for Exhaust Velocity given Gross Thrust in Turbojet, enter Gross Thrust of Turbojet (TG), Nozzle Exit Pressure (pe), Ambient Pressure (p∞), Nozzle Exit Area (Ae), Mass Flow Rate Turbojet (ma) & Fuel Air Ratio (f) and hit the calculate button. Here is how the Exhaust Velocity given Gross Thrust in Turbojet calculation can be explained with given input values -> 213.355 = (1124-(982-101)*0.0589)/(5*(1+0.008)).