How to Calculate Net Thrust Produced by Turbojet?
Net Thrust Produced by Turbojet calculator uses Net Thrust of Turbojet = Mass Flow Rate Turbojet*(1+Fuel Air Ratio)*(Exit Velocity-Flight Speed)+Nozzle Exit Area*(Nozzle Exit Pressure-Ambient Pressure) to calculate the Net Thrust of Turbojet, Net Thrust Produced by Turbojet formula is defined as the total thrust produced by a turbojet engine considering flight speed, exhaust speed, fuel-to-air ratio and mass flow rate of air. Net Thrust of Turbojet is denoted by T symbol.
How to calculate Net Thrust Produced by Turbojet using this online calculator? To use this online calculator for Net Thrust Produced by Turbojet, enter Mass Flow Rate Turbojet (ma), Fuel Air Ratio (f), Exit Velocity (Ve), Flight Speed (V), Nozzle Exit Area (Ae), Nozzle Exit Pressure (pe) & Ambient Pressure (p∞) and hit the calculate button. Here is how the Net Thrust Produced by Turbojet calculation can be explained with given input values -> 56.9309 = 5*(1+0.008)*(213-130)+0.0589*(982-101).