Equal to
Double
Three times
Six times
C. Three times
0.1 %
0.5 %
1 %
5 %
Before the intercooler
After the intercooler
Between the aftercooler and receiver
Before first stage suction
Isothermal
Polytropic
Isentropic
Any one of these
There is no pressure drop in the intercooler
The compression in both the cylinders is polytropic
The suction and delivery of air takes place at constant pressure
All of the above
200°C
500°C
700°C
1000°C
Reduced
Increased
Zero
None of these
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
20 - 30 %
40 - 50 %
60 - 70 %
70 - 90 %
7 : 1
15 : 1
30 : 1
50 : 1.
Forward curved
Backward curved
Radial
None of these
Closed cycle gas turbine is an I.C engine
Gas turbine uses same working fluid over and over again
Ideal efficiency of closed cycle gas turbine plant is more than Carnot cycle efficiency
Thrust in turbojet is produced by nozzle exit gases.
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, coke, anthracite coal or charcoal in a mixed air steam blast
1 bar
16 bar
64 bar
256 bar
Work done in first stage should be more
Work done in subsequent stages should increase
Work done in subsequent stages should decrease
Work done in all stages should be equal
Zero
Less
More
Same
Diffuser inlet radius
Diffuser outlet radius
Impeller inlet radius
Impeller outlet radius
These are used to dampen pulsations
These act as reservoir to take care of sudden demands
These increase compressor efficiency
These knock out some oil and moisture
Same
Lower
Higher
None of these
Increases
Decreases
Remains same
Increases/decreases depending on compressor capacity
The ratio of stroke volume to clearance volume
The ratio of the air actually delivered to the amount of piston displacement
Reciprocal of compression ratio
Index of compressor performance
Net work output and work done by turbine
Net work output and heat supplied
Work done by turbine and heat supplied
Work done by turbine and net work output
Less
More
Same
May be less or more depending on ambient conditions
Compressor efficiency
Isothermal efficiency
Volumetric efficiency
Mechanical efficiency
Lowest
Highest
Anything
Atmospheric
Compressor work and turbine work
Output and input
Actual total head temperature drop to the isentropic total head drop from total head inlet to static head outlet
Actual compressor work and theoretical compressor work
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
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
Increase of work ratio
Decrease of thermal efficiency
Decrease of work ratio
Both (A) and (B) above
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
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