1 bar
16 bar
64 bar
256 bar
C. 64 bar
Increases the thermal efficiency
Increases the compressor work
Increases the turbine work
Decreases the thermal efficiency
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
Vi = Vo
Vt > Vo
U < Vo
V = Uo
Gas turbine plant
Petrol engine
Diesel engine
Solar plant
Radial flow compressors
Axial flow compressors
Pumps
All of these
Less
More
Same
More/less depending on compressor capacity
Does not change
Increases
Decreases
First decrease and then increase
Equal to
Less than
More than
None of these
Same
Higher
Lower
None of these
Better lubrication is possible advantages of multistage
More loss of air due to leakage past the cylinder
Mechanical balance is better
Air can be cooled perfectly in between
Increase of work ratio
Decrease of thermal efficiency
Decrease of work ratio
Both (A) and (B) above
As large as possible
As small as possible
About 50% of swept volume
About 100% of swept volume
At very high speed
At very slow speed
At average speed
At zero speed
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
Start-stop motor
Constant speed unloader
Relief valve
Variable speed
Compressor efficiency
Volumetric efficiency
Isothermal efficiency
Mechanical efficiency
Carbonisation of coal
Passing steam over incandescent coke
Passing air and a large amount of steam over waste coal at about 65°C
Partial combustion of coal, eke, anthracite coal or charcoal in a mixed air steam blast
Atmospheric
Slightly more than atmospheric
Slightly less than atmospheric
Pressure slightly less than atmospheric and temperature slightly more than atmospheric
Less
More
Same
May be less or more depending upon speed
Decreases
Increases
Does not change
None of these
To cool the air during compression
To cool the air at delivery
To enable compression in two stages
To minimise the work of compression
Pressure ratio
Pressure coefficient
Degree of reaction
Slip factor
Isothermal h.p. to the BHP of motor
Isothermal h.p. to adiabatic h.p.
Power to drive compressor to isothermal h.p.
Work to compress air isothermally to work for actual compression
High nickel alloy
Stainless steel
Carbon steel
High alloy steel
It requires very big cylinder
It does not increase pressure much
It is impossible in practice
Compressor has to run at very slow speed to achieve it
Reduced volume flow rate
Increased volume flow rate
Lower suction pressure
Lower delivery pressure
Stainless steel
High alloy steel
Duralumin
Timken, Haste alloys
The compression ratio in each stage should be same
The intercooling should be perfect
The workdone in each stage should be same
All of the above
Same
More
Less
Zero
Thrust and range of aircraft
Efficiency of the engine
Both (A) and (B)
None of these