How to Calculate Exhaust Velocity given Thrust in Turbojet?
Exhaust Velocity given Thrust in Turbojet calculator uses Exit Velocity = (Net Thrust of Turbojet-Nozzle Exit Area*(Nozzle Exit Pressure-Ambient Pressure))/(Mass Flow Rate Turbojet*(1+Fuel Air Ratio))+Flight Speed to calculate the Exit Velocity, Exhaust Velocity given Thrust in Turbojet is defined as velocity of the exhaust gases leaving a turbojet engine. Exit Velocity is denoted by Ve symbol.
How to calculate Exhaust Velocity given Thrust in Turbojet using this online calculator? To use this online calculator for Exhaust Velocity given Thrust in Turbojet, enter Net Thrust of Turbojet (T), Nozzle Exit Area (Ae), Nozzle Exit Pressure (pe), Ambient Pressure (p∞), Mass Flow Rate Turbojet (ma), Fuel Air Ratio (f) & Flight Speed (V) and hit the calculate button. Here is how the Exhaust Velocity given Thrust in Turbojet calculation can be explained with given input values -> 294.7597 = (469-0.0589*(982-101))/(5*(1+0.008))+130.