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Nozzle thrust calculation

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Old   September 7, 2018, 06:27
Default Nozzle thrust calculation
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Bal Krishan
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Hi guys!

I have rocket nozzle simulated data, I want to calculate the thrust from that. One way is to calculate using the thrust equation at the exit. Is it possible to calculate the thrust using only nozzle pressure.
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Old   September 7, 2018, 19:05
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You would have to calculate an area integral of pressure over the exhaust plane.
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