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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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Rotary compressors are suitable for
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Surging is the phenomenon of
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The efficiency of the vane blower is (where W₁ = Workdone due to compression, and W₂ = Workdone due to back flow)
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Maximum delivery pressure is a rotary air compressor is of the order of
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Volumetric efficiency of a compressor decreases with ________ in compression ratio.
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The maximum compression ratio in an actual single stage axial flow compressor is of the order of
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