The knocking tendency in compression ignition engines for a given fuel will be Enhanced by increasing compression ratio Enhanced by decreasing compression ratio Dependent on other factors None of these TRUE ANSWER : ? YOUR ANSWER : ?
The compensating jet in a carburettor supplies almost constant amount of petrol at all speeds because the Jet area is automatically varied depending on the suction Flow is produced due to the static head in the float chamber The diameter of the jet is constant and the discharge coefficient is invariant The flow from the main jet is diverted to the compensating jet with increase in speed TRUE ANSWER : ? YOUR ANSWER : ?
The pressure at the end of compression, in petrol engines, is approximately 35 bar 20 bar 10 bar 25 bar TRUE ANSWER : ? YOUR ANSWER : ?
The tangential velocity of the water element having a free vortex is Directly proportional to its distance from the centre Directly proportional to its (distance)2 from the centre Inversely proportional to its (distance)2 from the centre Inversely proportional to its distance from the centre TRUE ANSWER : ? YOUR ANSWER : ?
The cetane (Câ‚₆H₃₄) which is a straight chain paraffin, is assigned a cetane number of 100 50 120 TRUE ANSWER : ? YOUR ANSWER : ?
In a four stroke cycle engine, the sequence of operations is Compression, expansion, suction and exhaust Suction, compression, expansion and exhaust Suction, expansion, compression and exhaust Expansion, compression, suction and exhaust TRUE ANSWER : ? YOUR ANSWER : ?
In petrol engines, advancing of the spark timing will ___ the knocking tendency. Not effect Decrease Increase None of the listed here TRUE ANSWER : ? YOUR ANSWER : ?
Stoichiometric ratio is Chemically correct air-fuel ratio by weight Actual air-fuel ratio for maximum efficiency None of these Chemically correct air-fuel ratio by volume TRUE ANSWER : ? YOUR ANSWER : ?
The purpose of testing an internal combustion engine is To conform the data used in design, the validity of which may be doubtful All of these To determine the information, which cannot be obtained by calculations To satisfy the customer regarding the performance of the engine TRUE ANSWER : ? YOUR ANSWER : ?
If Vâ‚ is the jet velocity and Vâ‚€ is the vehicle velocity, then propulsive efficiency of a turbojet engine is Vâ‚€ / (Vâ‚€ + Vâ‚) 2Vâ‚ / (Vâ‚€ + Vâ‚) Vâ‚ / (Vâ‚€ + Vâ‚) 2Vâ‚€ / (Vâ‚€ + Vâ‚) TRUE ANSWER : ? YOUR ANSWER : ?