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- Thrust calculation can be done using the following formulas12345:
- Thrust (F) = (Exit mass flow rate * Exit velocity) - (Free stream mass flow rate * Free stream velocity)
- Specific thrust (Fs) = (1 + fuel-air ratio) * Nozzle exit velocity - Free stream velocity
- Specific impulse = Thrust / Mass flow rate / Gravitational acceleration
Learn more:✕This summary was generated using AI based on multiple online sources. To view the original source information, use the "Learn more" links.The thrust is then equal to the exit mass flow rate times the exit velocity minus the free stream mass flow rate times the free stream velocity. F = (m dot * V)e – (m dot * V)0 The first term on the right hand side of this equation is usually called the gross thrust of the engine, while the second term is called the ram drag.www1.grc.nasa.gov/beginners-guide-to-aeronautic…The force (thrust) is equal to the exit mass flow rate times the exit velocity minus the free stream mass flow rate times the free stream velocity. Since the exit mass flow rate is nearly equal to the free stream mass flow rate, and the free stream is all air, we can call the mass flow rate through the engine the engine airflow rate.www.grc.nasa.gov/WWW/k-12/VirtualAero/BottleR…To calculate thrust, multiply the velocity by the mass flow rate (also known as change in mass divided by change in time).calculator.academy/thrust-calculator/The general thrust equation is given just below the graphic in the specific thrust form. Fs = F / m = (1 + mf) * Ve - V0 where Fs is the specific thrust, F is the net thrust, m is the air flow rate through the engine, mf is the fuel-air ratio, Ve is the nozzle exit velocity, and V0 is the free stream velocity.www.grc.nasa.gov/WWW/k-12/airplane/thsum.htmlTo calculate the specific impulse of an engine:
- Find the thrust produced by the engine.
- Divide the thrust with the mass flow rate.
- Divide the resultant with gravitational acceleration to obtain the specific impulse.
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