Mechanical Engineering :: Compressors, Gas Turbines and Jet Engines
- The ideal efficiency of simple gas turbine cycle depends on
- There is a certain pressure ratio (optimum) for a gas turbine at which its thermal efficiency is maximum. With increase in turbine temperature, the value of pressure ratio for the peak efficiency would
- Ratio of indicated h.p. to shaft h.p. in known as
- Ratio of indicated H.P. and brake H.P. is known as
- The output of a gas turbine is 300 KW and its efficiency is 20 percent, the heat supplied is
- Reheating in a gas turbine
- In axial flow compressor, exit flow angle deviation from the blade angle is a function of
- The air power of the compressor is also known as
- To avoid moisture troubles, the compressed air main line should
- The ratio of the discharge pressure to the inlet pressure of air is called
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