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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
OpenVideRime asked 3 years ago • 
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As the turbine inlet temperature increases, the thermal efficiency of gas turbine for the optimum pressure ratio
OpenVideRime asked 3 years ago • 
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The pressure of air at the beginning of the compression stroke is ________ the atmospheric pressure.
OpenVideRime asked 3 years ago • 
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The thermal efficiency of a simple gas turbine for a given turbine inlet temperature with increase in pressure ratio
OpenVideRime asked 3 years ago • 
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The ideal efficiency of simple gas turbine cycle depends on
OpenVideRime asked 3 years ago • 
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The ratio of specific weight/h.p. of gas turbine and I.C engines may be typically of the order of
OpenVideRime asked 3 years ago • 
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In a single stage, single acting reciprocating air compressor, without clearance volume, the work-done is minimum during
OpenVideRime asked 3 years ago • 
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Mechanical efficiency of gas turbines as compared to I.C engines is
OpenVideRime asked 3 years ago • 
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A closed cycle gas turbine works on
OpenVideRime asked 3 years ago • 
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Gas turbines for power generation are normally used
OpenVideRime asked 3 years ago • 
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