Half the operating speed
One fourth of operating speed
250 - 300 rpm
60 - 80 rpm
D. 60 - 80 rpm
Lean
Rich
Chemically correct
None of these
Equally efficient
Less efficient
More efficient
None of these
15 %
30 %
50 %
70 %
Fuel pump
Governor
Injector
Carburettor
Uniform throughout the mixture
Chemically correct mixture
About 35% of rich mixture
About 10% of rich mixture
Have no effect on
Increase
Decrease
None of these
Geometry of the reflector
Energy of neutrons
Properties of the reflector
All of these
In the engine cylinder
At the crank shaft
At the crank pin
None of these
Higher maximum temperature
Qualitative governing
Quantitative governing
Hit and miss governing
Thermal efficiency of diesel engine is about 34%
Theoretically correct mixture of air and petrol is approximately 15:1
High speed compression engines operate on dual combustion cycle
S.I. engines are quality governed engines
14.6 : 1
18.5 : 1
20.4 : 1
22.6 : 1
In compression ignition engines, detonation occurs near the beginning of combustion.
Since the fuel, in compression ignition engines, is injected at the end of compression stroke, therefore, there will be no pre-ignition.
To eliminate knock in compression ignition engines, we want to achieve auto-ignition not early and desire a long delay period.
In compression ignition engines, because of heterogeneous mixture, the rate of pressure rise is comparatively lower.
Low heat value of oil
High heat value of oil
Net calorific value of oil
Calorific value of fuel
Otto cycle is more efficient than the Diesel
Diesel cycle is more efficient than Otto
Both Otto and Diesel cycles are, equally efficient
Compression ratio has nothing to do with efficiency
2-stroke petrol engine
4-stroke petrol engine
Diesel engine
Steam turbine
6 to 10
10 to 15
15 to 25
25 to 40
Starts at 40° after bottom dead centre and ends at 30° before top dead centre
Starts at 40° before bottom dead centre and ends at 30° after bottom dead centre
Starts at bottom dead centre and ends at top dead centre
May start and end anywhere
25 %
50 %
70 %
100 %
0.2 kg
0.25 kg
0.3 kg
0.35 kg
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
Fuel pump
Fuel injector
Spark plug
None of these
Arrangement of the cylinders
Design of crankshaft
Number of cylinders
All of these
Kerosene
Gasoline
Paraffin
Natural gas
1 - rγ - 1
1 + rγ - 1
1 - (1/rγ - 1)
None of these
Benzene
Iso-octane
Normal heptane
Alcohol
500-1000°C
1000-1500°C
1500-2000°C
2000-2500°C
Cetane number 65
Octane number 65
Cetane number 35
Octane number 35
Low power will be produced
Efficiency will be low
Higher knocking will occur
Black smoke will be produced
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
0.2 kg
0.25 kg
0.3 kg
0.35 kg