Actual volume of the air delivered by the compressor when reduced to normal temperature and pressure conditions
Volume of air delivered by the compressor
Volume of air sucked by the compressor during its suction stroke
None of the above
A. Actual volume of the air delivered by the compressor when reduced to normal temperature and pressure conditions
Increases power output
Improves thermal efficiency
Reduces exhaust temperature
Do not damage turbine blades
1.03 kg/cm²
1.06 kg/cm²
1.00 kg/cm²
0.53 kg/cm²
10 to 40 %
40 to 60 %
60 to 70 %
70 to 90 %
6000 KW
15 KW
600 KW
150 KW
Injecting water into the compressor
Burning fuel after gas turbine
Injecting ammonia into the combustion chamber
All of the above
Vi = Vo
Vt > Vo
U < Vo
V = Uo
W₁/(W₁ + W₂)
W₂/(W₁ + W₂)
(W₁ + W₂)/W₁
(W₁ + W₂)/W₂
Remove impurities from air
Reduce volume of air
Cause moisture and oil vapour to drop out
Cool the air
Mass
Energy
Flow
Linear momentum
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
Employing intercooler
By constantly cooling the cylinder
By running compressor at very slow speed
By insulating the cylinder
Equal to
Less than
More than
None of these
Compression ratio
Expansion ratio
Compressor efficiency
Volumetric efficiency
Lower heating value
Higher heating value
Heating value
Higher calorific value
Rotor to static enthalpy rise in the stator
Stator to static enthalpy rise in the rotor
Rotor to static enthalpy rise in the stage
Stator to static enthalpy rise in the stage
Directly proportional to clearance volume
Greatly affected by clearance volume
Not affected by clearance volume
Inversely proportional to clearance volume
Diffuser inlet radius
Diffuser outlet radius
Impeller inlet radius
Impeller outlet radius
Low
High
Same
Low/high depending on make and type
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
Increase temperature
Reduce turbine size
Increase power output
Increase speed
Decreasing the compression work
Increasing the compression work
Increasing the turbine work
Both (A) and (C) above
Carnot cycle
Rankine cycle
Ericsson cycle
Joule cycle
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
Indicated power
Brake power
Frictional power
None of these
Vacuum
Atmospheric air
Compressed air
Oxygen alone
Centrifugal type
Axial flow type
Radial flow type
None of these
3.5 : 1
5 : 1
8 : 1
12 : 1
In two phases
In three phases
In a single phase
In the form of air and water mixture
Centrifugal compressor
Axial compressor
Pumps
All of the above
0.5 kg
1.0 kg
1.3 kg
2.2 kg