Question Category: Mechanical Engineering

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The ideal efficiency of simple gas turbine cycle depends on
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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
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In a single stage, single acting reciprocating air compressor, without clearance volume, the work-done is minimum during
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Mechanical efficiency of gas turbines as compared to I.C engines is
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A closed cycle gas turbine works on
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Gas turbines for power generation are normally used
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Stalling of blades in axial flow compressor is the phenomenon of
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The propulsive power of the rocket is (where v₁ = Jet velocity, and v₂ = Aircraft velocity)
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The volumetric efficiency of compressor with increase in compression ratio will
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For perfect intercooling in a two stage compressor
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