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Air at an absolute pressure 60.0 kPa and 27∘ enters a passage at 486 m/s. The cross sectional area at the entrance is 0.02 m2.
written 6.0 years ago by | • modified 4.9 years ago |
At section 2, further downstream, the pressure is 78.8 kPa(abs). Assuming isotropic flow. Calculate the mach no. at section 2. Also identify the type of nozzle.
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