How to Calculate Turbojet Gross Thrust?
Turbojet Gross Thrust calculator uses Gross Thrust of Turbojet = Mass Flow Rate Turbojet*(1+Fuel Air Ratio)*Exit Velocity+(Nozzle Exit Pressure-Ambient Pressure)*Nozzle Exit Area to calculate the Gross Thrust of Turbojet, Turbojet Gross Thrust formula is defined as total thrust produced by a turbojet excluding the ram drag. It is sum of momentum and pressure thrust. Gross Thrust of Turbojet is denoted by TG symbol.
How to calculate Turbojet Gross Thrust using this online calculator? To use this online calculator for Turbojet Gross Thrust, enter Mass Flow Rate Turbojet (ma), Fuel Air Ratio (f), Exit Velocity (Ve), Nozzle Exit Pressure (pe), Ambient Pressure (p∞) & Nozzle Exit Area (Ae) and hit the calculate button. Here is how the Turbojet Gross Thrust calculation can be explained with given input values -> 1122.216 = 5*(1+0.008)*213+(982-101)*0.0589.