Determine thrust produced by the nozzle in atmospheric air

Reference no: EM131346984

A sonic converging nozzle with a negligible inlet velocity and inlet and throat areas of 2.00 in² and 0.500 in² , respectively, has a velocity coefficient of 0.820 when the upstream stagnation pressure and temperature are 100. psia and 70.0°F.

Determine the thrust produced by the nozzle in atmospheric air.

Reference no: EM131346984

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