Air at a stagnation pressure of 1 MPa flows isentropically through a CD nozzle and exhausts into
Question:
Air at a stagnation pressure of 1 MPa flows isentropically through a CD nozzle and exhausts into ambient at 40.4 kPa. The edge of the jet, as it comes out of the nozzle is deflected by 18° (counter clockwise) from the horizontal. Determine the Mach number and static pressure at the nozzle exit.
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Step by Step Answer:
To determine the Mach number and static pressure at the nozzle exit we can use the isentropic flow r...View the full answer
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Muhammad Umair
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