Mechanical efficiency
Volumetric efficiency
Isothermal efficiency
Adiabatic efficiency
A. Mechanical efficiency
A.C. electric motor
Compressed air
Petrol engine
Diesel engine
In one cylinder
In two cylinders
In a single cylinder on both sides of the piston
In two cylinders on both sides of the piston
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
Large discharge at high pressure
Low discharge at high pressure
Large discharge at low pressure
Low discharge at low pressure
Compresses 3 m³/min of standard air
Compresses 3 m³/ min of free air
Delivers 3 m³/ min of compressed air
Delivers 3 m³/ min of compressed air at delivery pressure
Compression ratio
Expansion ratio
Compressor efficiency
Volumetric efficiency
Pressure ratio
Maximum cycle temperature
Minimum cycle temperature
All of the above
Slip factor
Velocity factor
Velocity coefficient
None of the above
No propeller
Propeller in front
Propeller at back
Propeller on the top
Air stream blocking the passage
Motion of air at sonic velocity
Unsteady, periodic and reversed flow
Air stream not able to follow the blade contour
Gas turbine plant
Petrol engine
Diesel engine
Solar plant
Power consumption per unit of air delivered is low
Volumetric efficiency is high
It is best suited for compression ratios around 7:1
The moisture in air is condensed in the intercooler
Equal to
Less than
More than
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
Low speeds
High speeds
Low altitudes
High altitudes
In a two stage reciprocating air compressor with complete intercooling, maximum work is saved.
The minimum work required for a two stage reciprocating air compressor is double the work required for each stage.
The ratio of the volume of free air delivery per stroke to the swept volume of the piston is called volumetric efficiency.
None of the above
(p₁ - p₂)/2
(p₁ + p₂)/2
p₁/p₂
p₁ p₂
Increases with decrease in compression ratio
Decreases with decrease in compression ratio
Increases with increase in compression ratio
Decreases with increase in compression ratio
The atmosphere
A source at 0°C
A source of low temperature air
A source of high temperature air
Provides greater flexibility
Provides lesser flexibility
In never used
Is used when gas is to be burnt
It is inefficient
It is bulky
It requires cooling water for its operation
None of the above
Paucity of O2
Increasing gas temperature
High specific volume
High friction losses
In gas turbine plants
For operating pneumatic drills
In starting and supercharging of I.C. engines
All of the above
Surrounding air
Compressed atmospheric air
Its own oxygen
None of these
p₂/p₁ = p₃/p₂ = p₄/p₃
p₃/p₁ = p₄/p₂
p₁ p₂ = p₃ p₄
p₁ p₃ = p₂ p₄
Centrifugal compressor
Axial compressor
Pumps
All of the above
Is self operating at zero flight speed
Is not self operating at zero flight speed
Requires no air for its operation
Produces a jet consisting of plasma
1 to 5 bar
5 to 8 bar
8 to 10 bar
10 to 15 bar
30 : 1
40 : 1
50 : 1
60 : 1
Employing intercooler
By constantly cooling the cylinder
By running compressor at very slow speed
By insulating the cylinder