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
A. Large quantity of air at high pressure
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 with increase in compression ratio
Decreases with increase in compression ratio
In not dependent upon compression ratio
May increase/decrease depending on compressor capacity
Free air delivery
Compressor capacity
Swept volume
None of these
30 : 1
40 : 1
50 : 1
60 : 1
Decrease
Increase
Remain same
Does not change
Before intercooler
After intercooler
After receiver
Between after-cooler and air receiver
Requires less space for installation
Has compressor and combustion chamber
Has less efficiency
All of these
Increase
Decrease
Remain same
May increase or decrease depending on clearance volume
Large discharge at high pressure
Low discharge at high pressure
Large discharge at low pressure
Low discharge at low pressure
Inlet whirl velocity
Outlet whirl velocity
Inlet velocity of flow
Outlet velocity of flow
One adiabatic, two isobaric, and one constant volume
Two adiabatic and two isobaric
Two adiabatic, one isobaric and one constant volume
One adiabatic, one isobaric and two constant volumes
From an air conditioned room maintained at 20°C
From outside atmosphere at 1°C
From coal yard side
From a side where cooling tower is located nearby
1 : 1
2 : 1
4 : 1
1 : 6
Increase of work ratio
Decrease of thermal efficiency
Decrease of work ratio
Both (A) and (B) above
Compression index
Compression ratio
Compressor efficiency
Mean effective pressure
Gas turbine
I.C engine
Compressor
Air motor
Increase in net output but decrease in thermal efficiency
Increase in thermal efficiency but decrease in net output
Increase in both thermal efficiency and net output
Decrease in both thermal efficiency and net output
Isothermal compression
Adiabatic compression
Isentropic compression
Polytropic compression
One stroke
Two strokes
Three strokes
Four strokes
Radial component
Axial component
Tangential component
None of the above
Injecting water into the compressor
Burning fuel after gas turbine
Injecting ammonia into the combustion chamber
All of the above
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
Indicated power
Brake power
Frictional power
None of these
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
Gas turbine requires lot of cooling water
Gas turbine is capable of rapid start up and loading
Gas turbines has flat efficiency at part loads
Gas turbines have high standby losses and require lot of maintenance
p₂ = p₁ × p₃
p₂ = p₁/p₃
p₂ = p₁ × p₂
p₂ = p₃/p₁
Mass
Energy
Flow
Linear momentum
Stainless steel
High alloy steel
Duralumin
Timken, Haste alloys
Turbojet engine
Ramjet engine
Propellers
Rockets
Pressure ratio
Maximum cycle temperature
Minimum cycle temperature
All of the above