Isothermal
Polytropic
Isentropic
Any one of these
D. Any one of these
Free air delivery
Compressor capacity
Swept volume
None of these
Increases
Decreases
Remains same
Increases/decreases depending on compressor capacity
Reciprocating compressor
Centrifugal compressor
Axial flow compressor
Turbo compressor
Constant volume
Constant temperature
Constant pressure
None of these
The flow of air is parallel to the axis of the compressor
The static pressure of air in the impeller increases in order to provide centripetal force on the air
The impeller rotates at high speeds
The maximum efficiency is higher than multistage axial flow compressors
Large quantity of air at high pressure
Small quantity of air at high pressure
Small quantity of air at low pressure
Large quantity of air at low pressure
Forward curved
Backward curved
Radial
None of these
Requires less space for installation
Has compressor and combustion chamber
Has less efficiency
All of these
(p₁ - p₂)/2
(p₁ + p₂)/2
p₁/p₂
p₁ p₂
Has no effect on
Decreases
Increases
None of these
Less
More
Same
May be less or more depending upon speed
Atmospheric conditions at any specific location
20°C and 1 kg/cm² and relative humidity of 36%
0°C and standard atmospheric conditions
15°C and 1 kg/cm²
Atmospheric
Slightly more than atmospheric
Slightly less than atmospheric
Pressure slightly less than atmospheric and temperature slightly more than atmospheric
1 - k + k (p₁/p₂)1/n
1 + k - k (p₂/p₁)1/n
1 - k + k (p₁/p₂) n- 1/n
1 + k - k (p₂/p₁) n-1/n
Increases the thermal efficiency
Increases the compressor work
Increases the turbine work
Decreases the thermal efficiency
Increases
Decreases
Remain unaffected
May increase or decrease depending on compressor capacity
Large discharge at high pressure
Low discharge at high pressure
Large discharge at low pressure
Low discharge at low pressure
Isothermal compression
Adiabatic compression
Isentropic compression
Polytropic compression
Gas turbine
4-stroke petrol engine
4-stroke diesel engine
Multi cylinder engine
Compressor
Heating chamber
Cooling chamber
All of these
It has high propulsive efficiency at high speeds
It can fly at supersonic speeds
It can fly at high elevations
It has high power for take off
More power
Less power
Same power
More/less power depending on other factors
Vacuum
Atmospheric air
Compressed air
Oxygen alone
Centrifugal compressor
Axial compressor
Pumps
All of the above
0.1 to 1.2 m³/s
0.15 to 5 m³/s
Above 5 m³/s
None of these
Jet velocity
Twice the jet velocity
Half the jet velocity
Average of the jet velocity
7 : 1
15 : 1
30 : 1
50 : 1.
Start-stop motor
Constant speed unloader
Relief valve
Variable speed
Same
Higher
Lower
Dependent on other factors
The ratio of the discharge pressure to the inlet pressure of air is called compressor efficiency
The compression ratio for the compressor is always greater than unity
The compressor capacity is the ratio of workdone per cycle to the stroke volume
During isothermal compression of air, the workdone in a compressor is maximum