The upstream stagnation pressure and temperature are 0150, Physics

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The upstream stagnation pressure and temperature are 0150

Experimental measurements on a new methane fuel nozzle for a furnace produce an exit velocity, pressure, and temperature for methane of 335 m/s, 0.100 MPa, and 0.00°C. The upstream stagnation pressure and temperature are 0.150 MPa and 22.0°C. Determine

a. The nozzle efficiency.

b. The nozzle's velocity coefficient.

c. The nozzle's discharge coefficient.

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Physics: The upstream stagnation pressure and temperature are 0150

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Physics: The upstream stagnation pressure and temperature are 0150

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