Find the actual compressor work and its exit temperature
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A steam turbine inlet is at 200 psia, 800 F. The exit is at 40 psia. What is the highest possible exit temperature? Which efficiency does that correspond to?
The inlet temperature is 1800 R, and it exhausts to the atmosphere. Find the required inlet pressure and the exhaust temperature.
The isentropic efficiency may be assumed to be 90%. What pressure and temperature are required in the line upstream of the nozzle?
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Find the actual compressor work and its exit temperature and find the actual nozzle exit velocity.
What type of times interest earned ratio would be desirable? What type would not be desirable?
Compute the heat transfer to the tank and show that this process does not violate the second law.
Power input to the pump is 3 Btu/s. Assuming the pump process to be reversible, compute the pump exit pressure and temperature.
What is the pressure at the front stagnation point that is 6 ft down from the water surface?
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