Gas turbine uses low air-fuel ratio to economise on fuel
Gas turbine uses high air-fuel ratio to reduce outgoing temperature
Gas turbine uses low air-fuel ratio to develop the high thrust required
All of the above
B. Gas turbine uses high air-fuel ratio to reduce outgoing temperature
Reduction of speed of incoming air and conversion of part of it into pressure energy
Compression of inlet air
Increasing speed of incoming air
Lost work
Vi = Vo
Vt > Vo
U < Vo
V = Uo
Isothermally
Adiabatically
Isentropically
Isochronically
Temperature during compression remains constant
No heat leaves or enters the compressor cylinder during compression
Temperature rise follows a linear relationship
Work done is maximum
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
Low speeds
High speeds
Low altitudes
High altitudes
Provides greater flexibility
Provides lesser flexibility
In never used
Is used when gas is to be burnt
Electric motor
Engine
Either (A) or (B)
None of these
A.C. electric motor
Compressed air
Petrol engine
Diesel engine
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
To accommodate Valves in the cylinder head
To provide cushioning effect
To attain high volumetric efficiency
To provide cushioning effect and also to avoid mechanical bang of piston with cylinder head
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
Equal to
Less than
More than
None of these
Free air delivery
Compressor capacity
Swept volume
None of these
Compressor efficiency
Isothermal efficiency
Volumetric efficiency
Mechanical efficiency
Same
One-half
One fourth
One sixth
Compressor efficiency
Isentropic efficiency
Euler's efficiency
Pressure coefficient
Large discharge at high pressure
Low discharge at high pressure
Large discharge at low pressure
Low discharge at low pressure
Gas turbine
4-stroke petrol engine
4-stroke diesel engine
Multi cylinder engine
Zero
Less
More
Same
1 : 1
2 : 1
4 : 1
1 : 6
Indicated power
Brake power
Frictional power
None of these
Has no effect on
Decreases
Increases
None of these
Isothermally
Polytropically
Isentropically
None of these
The reciprocating compressors are best suited for high pressure and low volume capacity
The effect of clearance volume on power consumption is negligible for the same volume of discharge
Both (A) and (B)
None of these
Constant volume
Constant temperature
Constant pressure
None of these
Atmosphere
Vacuum
Discharge nozzle
Back to the compressor
Compressor efficiency
Volumetric efficiency
Isothermal efficiency
Mechanical efficiency
High calorific value
Ease of atomisation
Low freezing point
Both (A) and (C) above
Toughness
Fatigue
Creep
Corrosion resistance