Cetane number
Octane number
Calorific value
All of these
B. Octane number
B.P = (Wl × 2πN)/60 watts
B.P = [(W - S) πDN]/60 watts
B.P = [(W - S) π (D + d) N]/60 watts
All of these
Fuel used
Speed of engine
Compression ratio
None of these
8 : 1
10 : 1
15 : 1
20 : 1 and less
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 %
4 %
8 %
14 %
1000 km/h
2000 km/h
2400 km/h
3000 km/h
Inlet valve closing after bottom dead centre
Inlet valve closing before bottom dead centre
Inlet valve opening before top dead centre
Exhaust valve closing after top dead centre
Scavenging
Detonation
Supercharging
Polymerisation
V₁/(V₀ + V₁)
V₀/(V₀ + V₁)
2V₀/(V₀ + V₁)
2V₁/(V₀ + V₁)
Hit and miss governing
Qualitative governing
Quantitative governing
Combination of (B) and (C)
0
50
100
120
Equal to
Below
Above
None of these
Same
Less
More
None of these
Flat
Contoured
Slanted
Depressed
Opens at 15° after top dead centre and closes at 20° before bottom dead centre
Opens at 15° before top dead centre and closes at 20° after top dead centre
Opens at top dead centre and closes at bottom dead centre
May open and close anywhere
Instantaneous and rapid burning of the first part of the charge
Instantaneous auto ignition of last part of charge
Delayed burning of the first part of the charge
Reduction of delay period
Fuel pump
Injector
Carburettor
None of these
Opens at 50° before bottom dead centre and closes at 15° after top dead centre
Opens at bottom dead centre and closes at top dead centre
Opens at 50° after bottom dead centre and closes at 15° before top dead centre
May open and close anywhere
Lean
Rich
Chemically correct
None of these
Napthene
Tetra ethyl lead
Amyl nitrate
Hexadecane
Theoretical power
Actual power
Indicated power
None of these
Have no effect on
Increase
Decrease
None of these
Enhance flow rate
Control air flow
Induce primary swirl
Induce secondary turbulence
A supercharger
A centrifugal blower
A vacuum chamber
An injection tube
Temperature and pressure in the cylinder at the time of injection
Nature of the fuel mixture strength
Relative velocity between the fuel injection and air turbulence pressure of residual gases
All of the above
2-stroke cycle engines
4-stroke cycle engines
Aeroplane engines
High efficiency engines
Otto cycle
Diesel cycle
Dual cycle
Carnot cycle
First a mild explosion followed by a bi explosion
First a big explosion followed by a mil explosion
Both mild and big explosions occurs simultaneously
Never occurs
0.15 kg
0.2 kg
0.25 kg
0.3 kg
0.2 kg
0.25 kg
0.3 kg
0.35 kg