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Thrust calculation from cfd data(Numerical Integration)

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Old   April 23, 2018, 06:18
Default Thrust calculation from cfd data(Numerical Integration)
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Bal Krishan
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I am doing CFD analysis on the supersonic nozzle, I need to calculate the thrust of the nozzle from CFD data. I don't know how to calculate the thrust numerically. The equation for thrust calculation is
T = \int \rho u (u.n) dA

please help
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