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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The compression ratio for the compressor is always _________ unity.

Equal to
None of these
More than
Less than

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Compressors, Gas Turbines and Jet Engines
The pressure ratio in gas turbines is of the order of

0.084027777777778
0.37569444444444
2.5423611111111
0.16736111111111

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Compressors, Gas Turbines and Jet Engines
In a reciprocating air compressor, the compression work per kg of air

Increases as clearance volume increases
Decreases as clearance volume increases
Increases as clearance volume decreases
Is independent of clearance volume

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Compressors, Gas Turbines and Jet Engines
The inter-cooler pressure, for minimum work required, for a two stage reciprocating air compressor, is given by (where p₁ = Intake pressure of air, p₂ = Inter-cooler pressure, and p₃ = Delivery pressure of air)

p₂ = p₃/p₁
p₂ = p₁ × p₂
p₂ = p₁ × p₃
p₂ = p₁/p₃

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Compressors, Gas Turbines and Jet Engines
The blades of gas turbine are made of

High nickel alloy
Stainless steel
Carbon steel
High alloy steel

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Compressors, Gas Turbines and Jet Engines
Maximum delivery pressure is a rotary air compressor is of the order of

16 kg/cm²
10 kg/cm²
25 kg/cm²
6 kg/cm²

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