Question Category: Compressors Gas Turbines and Jet Engines

Questions › Category: Compressors Gas Turbines and Jet Engines
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The output of a gas turbine is 300 KW and its efficiency is 20 percent, the heat supplied is
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An after-cooler is used to
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The pressure ratio in gas turbines is of the order of
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Inter-cooling in multistage compressors is done
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The air-fuel ratio in gas turbines is of the order of
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A large clearance volume in a reciprocating compressor results in
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The thermal efficiency of a gas turbine as compared to a diesel plant is
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Which of the following statement is correct relating to rocket engines?
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The degree of reaction in an axial flow compressor is defined as the ratio of static enthalpy rise in the
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The fuel consumption in gas turbines is accounted for by
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