How to Calculate Momentum Thrust?
Momentum Thrust calculator uses Ideal Thrust = Mass Flow Rate*((1+Fuel Air Ratio)*Exit Velocity-Flight Speed) to calculate the Ideal Thrust, Momentum Thrust formula is defined as the thrust produced due to change in momentum of the aircraft, discarding the thrust produced due to pressure. Ideal Thrust is denoted by Tideal symbol.
How to calculate Momentum Thrust using this online calculator? To use this online calculator for Momentum Thrust, enter Mass Flow Rate (ma), Fuel Air Ratio (f), Exit Velocity (Ve) & Flight Speed (V) and hit the calculate button. Here is how the Momentum Thrust calculation can be explained with given input values -> 487.312 = 3.5*((1+0.009)*248-111).