Diesel engines
Gas turbines
Petrol engines
Aircraft engines
D. Aircraft engines
Net efficiency
Efficiency ratio
Relative efficiency
Overall efficiency
Equal to
Below
Above
None of these
Not run
Run more efficiently
Run at high speed
Explode
Vaporisation
Carburetion
Ionisation
Atomisation
1 valve
2 valves
3 valves
4 valves
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
Clearance volume
Volumetric efficiency
Ignition time
Effective compression ratio
Cetane and iso-octane
Cetane and alpha-methyl naphthalene
Cetane and normal heptane
Cetane and tetra ethyl lead
Half
Same
Double
Four times
Arrangement of the cylinders
Design of crankshaft
Number of cylinders
All of these
Low
Very low
High
Very high
80°C
120°C
180°C
240°C
Pre-ignition period
Delay period
Period of ignition
Burning period
Remain same
Decrease
Increase
None of these
Mechanical efficiency
Overall efficiency
Indicated thermal efficiency
Volumetric efficiency
Detonation
Turbulence
Pre-ignition
Supercharging
180°
125°
235°
200°
A supercharger
A centrifugal blower
A vacuum chamber
An injection tube
Diesel engines
Gas turbines
Petrol engines
Aircraft engines
Calorific value of oil
Low heat value of oil
High heat value of oil
Mean heat value of oil
20 to 40
40 to 60
60 to 80
80 to 100
Piston ring and cylinder wear
Formation of hard coating on piston skirts
Oil sludge in the engine crank case
Detonation
Larger
Slowed down
Smaller
Liquid
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
Highly ignitable
More difficult to ignite
Less difficult to ignite
None of these
Uniform throughout the mixture
Chemically correct mixture
About 35% of rich mixture
About 10% of rich mixture
To reduce mass of the engine per brake power
To reduce space occupied by the engine
To increase the power output of an engine when greater power is required
All of the above
Kerosene
Gasoline
Paraffin
Natural gas
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
Diesel
Kerosene
Fuel oil
Gasoline