Question Category: Compressors Gas Turbines and Jet Engines

Questions › Category: Compressors Gas Turbines and Jet Engines
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Propulsive efficiency is defined as ratio of
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Which of the following fuels can be used in turbojet engines?
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A jet engine works on the principle of conservation of
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In the cross compounding of the gas turbine plant
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Choose the correct statement (A) Gas turbine requires lot of cooling water (B) Gas turbine is capable of rapid start up and loading 
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A closed gas turbine in which fuel is burnt directly in the air is not possible because of
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The power available for takeoff and climb in case of turbojet engine as compared to reciprocating engine is
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Pick up the wrong statement (A) Large gas turbines employ axial flow compressors (B) Axial flow compressors are more stable than centrifugal type compressors but not as efficient (C) Axial flow compressors have high capacity and efficiency
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The degree of reaction of an axial flow turbine is the ratio of isentropic temperature drop in a blade row to the
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In the axial flow gas turbine, the work ratio is the ratio of
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