A de Laval nozzle is to be designed to operate supersonically and expand ideally to an
Chapter 12, Problem 12.49(choose chapter or problem)
A de Laval nozzle is to be designed to operate supersonically and expand ideally to an absolute pressure of 25 kPa. If the stagnation pressure in the nozzle is 1 MPa, calculate the nozzle area ratio required. Determine the nozzle throat area for a mass flow of 10 kg/sand a stagnation temperature of 550 K. Assume that the gas is nitrogen.
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