Highly heated atmospheric air
Solids
Liquid
Plasma
A. Highly heated atmospheric air
Increase
Decrease
Remain same
May increase or decrease depending on clearance volume
Ammonia and water vapour
Carbon dioxide
Nitrogen
Hydrogen
10 to 40 %
40 to 60 %
60 to 70 %
70 to 90 %
Isothermally
Polytropically
Isentropically
None of these
Increase temperature
Reduce turbine size
Increase power output
Increase speed
Radial flow
Axial flow
Centrifugal
None of the above
p₂/p₁ = p₃/p₂ = p₄/p₃
p₃/p₁ = p₄/p₂
p₁ p₂ = p₃ p₄
p₁ p₃ = p₂ p₄
Large gas turbines employ axial flow compressors
Axial flow compressors are more stable than centrifugal type compressors but not as efficient
Axial flow compressors have high capacity and efficiency
Axial flow compressors have instability region of operation
Parallel
Perpendicular
Inclined
None of these
Paucity of O2
Increasing gas temperature
High specific volume
High friction losses
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
Same
More
Less
Depends on other factors
20 - 30 %
40 - 50 %
60 - 70 %
70 - 90 %
Atmospheric
Slightly more than atmospheric
Slightly less than atmospheric
Pressure slightly less than atmospheric and temperature slightly more than atmospheric
Increase
Decrease
Remain unaffected
Other factors control it
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
Gas turbine
I.C engine
Compressor
Air motor
D₁/D₂ = p₁ p₂
D₁/D₂ = p₁/p₂
D₁/D₂ = p₂/p₁
None of these
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
r -1
1 - r -1
1 - (1/r) -1/
1 - (1/r) /-1
Mechanical efficiency
Volumetric efficiency
Isothermal efficiency
Adiabatic efficiency
Centrifugal pump
Reciprocating pump
Turbine
Sliding vane compressor
p₂ = p₁ × p₃
p₂ = p₁/p₃
p₂ = p₁ × p₂
p₂ = p₃/p₁
At very high speed
At very slow speed
At average speed
At zero speed
It allows maximum compression to be achieved
It greatly affects volumetric efficiency
It results in minimum work
It permits isothermal compression
Mass flow rate
Pressure ratio
Change in load
Stagnation pressure at the outlet
1.03 kg/cm²
1.06 kg/cm²
1.00 kg/cm²
0.53 kg/cm²
Decreases net output but increases thermal efficiency
Increases net output but decreases thermal efficiency
Decreases net output and thermal efficiency both
Increases net output and thermal efficiency both
Compressor efficiency
Isothermal efficiency
Volumetric efficiency
Mechanical efficiency
Gas turbine plant
Petrol engine
Diesel engine
Solar plant