10 : 1
15 : 1
20 : 1
25 : 1
B. 15 : 1
Up to 35%
Up to 50%
Up to 75%
Up to 100%
Same
Lower
Higher
None of these
0.2 kg
0.25 kg
0.3 kg
0.35 kg
Jet area is automatically varied depending on the suction
The flow from the main jet is diverted to the compensating jet with increase in speed
The diameter of the jet is constant and the discharge coefficient is invariant
Flow is produced due to the static head in the float chamber
It is properly designed
Best quality fuel is used
Cannot work as it is impossible
Flywheel size is proper
Temperature
Volume
Density
None of these
Air only
Diesel only
A mixture of diesel and air
None of these
Fuel pump
Governor
Injector
Carburettor
Otto cycle
Diesel cycle
Dual cycle
Carnot cycle
Decrease
Increase
Remain same
None of these
Same
More
Less
Less or more depending on operating conditions
Increase
Reduce
Not effect
None of these
180°
125°
235°
200°
0
50
100
120
Starts at 40° after bottom dead centre and ends at 10° before top dead centre
Starts at 40° before top dead centre and ends at 40° after top dead centre
Starts at top dead centre and ends at 40° before bottom dead centre
May start and end anywhere
Clearance volume
Volumetric efficiency
Ignition time
Effective compression ratio
Kerosene
Gasoline
Paraffin
Natural gas
V₁/(V₀ + V₁)
V₀/(V₀ + V₁)
2V₀/(V₀ + V₁)
2V₁/(V₀ + V₁)
2000 to 4000 volts
4000 to 6000 volts
6000 to 10,000 volts
10,000 to 12,000 volts
Compression starts at 35° after bottom dead center and ends at top dead center
Compression starts at bottom dead center and ends at top dead center
Compression starts at 10° before bottom dead center and, ends just before top dead center
May start and end anywhere
Enhanced by decreasing compression ratio
Enhanced by increasing compression ratio
Dependent on other factors
None of the above
6 to 10
10 to 15
15 to 25
25 to 40
Theoretical power
Actual power
Indicated power
None of these
Cetane number
Octane number
Calorific value
None of these
Highly ignitable
More difficult to ignite
Less difficult to ignite
None of these
1 - rγ - 1
1 + rγ - 1
1 - (1/rγ - 1)
None of these
20 to 40
40 to 60
60 to 80
80 to 100
2-stroke engine can run in any direction
In 4-stroke engine, a power stroke is obtained in 4-strokes
Thermal efficiency of 4-stroke engine is more due to positive scavenging
Petrol engines occupy more space than diesel engines for same power output
14.6 : 1
18.5 : 1
20.4 : 1
22.6 : 1
Petrol engines
Diesel engines
Multi cylinder engines
All of these