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 is a measure of the forward force exerted by a turbojet engine, which is influenced by the mass flow rate, exhaust velocity, and pressure difference between the exit and ambient conditions, and is a critical parameter in the design and operation of aircraft and other propulsion systems. 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).