1/2
1
2
4
C. 2
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
Same
Less
More
None of these
6 kg/cm
12 kg/cm
20 kg/cm
35 kg/cm
Minimum temperature to which oil is heated in order to give off inflammable vapours in sufficient quantity to ignite momentarily when brought in contact with a flame
Temperature at which it solidifies or congeals
Temperature at which it catches fire without external aid
Indicated by 90% distillation temperature, i.e. when 90% of sample oil has distilled off
1 m3
5 m3
56 m3
910 m3
Low density
Low temperature
Long ignition delay
All of these
Alcohol
Water
Lead
None of these
0.3 kg/hr
1 kg/hr
3 kg/hr
5 kg/hr
Higher heating value
Higher flash point
Lower volatility
Longer ignition delay
6 to 10
10 to 15
15 to 25
25 to 40
To determine the information, which cannot be obtained by calculations
To conform the data used in design, the validity of which may be doubtful
To satisfy the customer regarding the performance of the engine
All of the above
Otto cycle
Diesel cycle
Dual combustion cycle
All of these
Arrangement of the cylinders
Design of crankshaft
Number of cylinders
All of these
Beginning of suction stroke
End of suction stroke
End of compression stroke
None of these
2 %
4 %
8 %
14 %
Peak pressure
Rate of rise of pressure
Rate of rise of temperature
Peak temperature
More
Less
Same
More/less depending on capacity of engine
Speed
Temperature
Volume of cylinder
m.e.p. and I.H.P.
Geometry of the reflector
Energy of neutrons
Properties of the reflector
All of these
40% cetane and 60% alpha methyl naphthalene
40% alpha methyl naphthalene and 60% cetane
40% petrol and 60% diesel
40% diesel and 60% petrol
Thermal efficiency
Speed
Power output
Fuel consumption
Equal to
Less than
Greater than
None of these
Diesel
Kerosene
Fuel oil
Gasoline
Transformer
D.C. generator
Capacitor
Magnetic circuit
Mechanical efficiency
Overall efficiency
Volumetric efficiency
Relative efficiency
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
Leaking piston rings
Use of thick head gasket
Clogged air inlet slots
All of the above
Air alone
Air and fuel
Air and lub oil
Fuel alone
It is properly designed
Best quality fuel is used
Cannot work as it is impossible
Flywheel size is proper
6 to 10
10 to 15
15 to 25
25 to 40