Show that the thrust developed by a stationary rocket motor


Show that the thrust developed by a stationary rocket motor is F = rho*A*U^2 + A(p- p_atm) where p_atm is the atmospheric pressure, and p, rho, A, and U are, respectively, the pressure, density, area, and velocity of the fluid at the nozzle exit.

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Mechanical Engineering: Show that the thrust developed by a stationary rocket motor
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