Explore topic-wise MCQs in Testing Subject.

This section includes 657 Mcqs, each offering curated multiple-choice questions to sharpen your Testing Subject knowledge and support exam preparation. Choose a topic below to get started.

1.

A nuclear power plant differs from a conventional steam power station only in the steam generating part.

A. Agree
B. Disagree
Answer» B. Disagree
2.

In a four stroke engine, the working cycle is completed in

A. one revolution of the crankshaft
B. two revolutions of the crankshaft
C. three revolutions of the crankshaft
D. four revolutions of the crankshaft
Answer» C. three revolutions of the crankshaft
3.

Which one of the following event would reduce volumetric efficiency of a vertical compression ignition engine ?

A. inlet valve closing after bottom dead centre
B. inlet valve closing before bottom dead centre
C. inlet valve opening before top dead centre
D. exhaust valve closing after top dead centre
Answer» C. inlet valve opening before top dead centre
4.

The efficiency of roots blower __________ with the increase in pressure ratio.

A. decreases
B. increases
C. does not change
Answer» B. increases
5.

The operation of lifts, rams and pumps make use of compressed air.

A. Yes
B. No
Answer» B. No
6.

In a compressed air system, the temperature of air discharged from the air motor is __________ than the initial compressor intake temperature.

A. more
B. less
Answer» C.
7.

Which of the following statement is correct relating to rocket engines ?

A. The combustion chamber in a rocket engine is directly analogous to the reservoir of a super sonic wind tunnel
B. The stagnation conditions exist at the combustion chamber
C. The exit velocities of exhaust gases are much higher than those in jet engine
D. all of the above
Answer» E.
8.

In reciprocating air compressors, isothermal efficiency is used for all sorts of calculations.

A. Correct
B. Incorrect
Answer» B. Incorrect
9.

Euler's equation can be used for

A. radial flow compressors
B. axial flow compressors
C. pumps
D. all of these
Answer» E.
10.

A jet engine has

A. no propeller
B. propeller in front
C. propeller at back
D. propeller on the top
Answer» B. propeller in front
11.

A rocket engine uses __________ for the combustion of its fuel.

A. surrounding air
B. compressed atmospheric air
C. its own oxygen
D. none of these
Answer» D. none of these
12.

Free air is the air at atmospheric conditions at any specific location.

A. True
B. False
Answer» B. False
13.

The perfect intercooling, in multistage compression, means that the temperature of air at inlet to subsequent stages is equal to the initial temperature.

A. Agree
B. Disagree
Answer» B. Disagree
14.

A gas turbine used in air-craft should have low weight and small frontal area.

A. Correct
B. Incorrect
Answer» B. Incorrect
15.

A closed cycle gas turbine works on

A. Carnot cycle
B. Rankine cycle
C. Ericsson cycle
D. Joule cycle
Answer» E.
16.

Air motors work on the cycle which is the reverse of the reciprocating air compressor cycle.

A. Agree
B. Disagree
Answer» B. Disagree
17.

The axial flow compressor is preferred in air-craft gas turbines because of

A. low frontal area
B. higher thrust
C. high pressure rise
D. none of these
Answer» B. higher thrust
18.

Which of the following statement is correct as regard to centrifugal compressors?

A. The flow of air is parallel to the axis of the compressor.
B. The static pressure of air in the impeller increases in order to provide centripetal force on the air.
C. The impeller rotates at high speeds.
D. The maximum efficiency is higher than multi-stage axial flow compressors.
Answer» C. The impeller rotates at high speeds.
19.

The ratio of the net work obtained from the gas turbine plant to the turbine work is known as

A. compression ratio
B. work ratio
C. pressure ratio
D. none of these
Answer» C. pressure ratio
20.

The clearance, in a single stage, single acting reciprocating air compressor does not effect the workdone on the air and the power required for compressing the air.

A. True
B. False
Answer» B. False
21.

The process, which causes the air to enter the impeller blades of a centrifugal compressor at __________ velocity (without effecting the mass of air to flow and velocity of flow) is known as prewhirl.

A. reduced
B. increased
Answer» B. increased
22.

A closed cycle gas turbine consists of a

A. compressor
B. heating chamber
C. cooling chamber
D. all of these
Answer» E.
23.

A receiver in compressor installations is used to damp pressure waves in compressor discharge.

A. Yes
B. No
Answer» B. No
24.

In jet propulsion power unit, the inlet duct of diverging shape is used for converting kinetic energy of air into pressure energy.

A. True
B. False
Answer» B. False
25.

For maximum work, the reheating should be done to an intermediate pressure of (where p1 = Maximum pressure, and p2 = Minimum pressure)

A. <img src="/_files/images/mechanical-engineering/compressors-gas-dynamics-and-gas-turbines/380-170-1.png">
B. <img src="/_files/images/mechanical-engineering/compressors-gas-dynamics-and-gas-turbines/380-170-2.png">
C. <img src="/_files/images/mechanical-engineering/compressors-gas-dynamics-and-gas-turbines/380-170-3.png">
D. <span class="root"><i>p</i><sub>1</sub><i>p</i><sub>2</sub></span>
Answer» E.
26.

The temperature of air at the beginning of the compression stroke is __________ the atmospheric temperature.

A. equal to
B. less than
C. more than
Answer» D.
27.

The pressure ratio in a centrifugal compressor can be increased by increasing the tip speed and lowering the inlet temperature.

A. Correct
B. Incorrect
Answer» B. Incorrect
28.

Gas turbine as compared to internal combustion engine

A. can be driven at a very high speed
B. produces uniform torque
C. has more efficiency
D. all of these
Answer» E.
29.

A two stroke cycle engine occupies larger floor area than a four stroke cycle engine.

A. Yes
B. No
Answer» C.
30.

The compressor efficiency is defined as the ratio of volume of free air delivery per stroke to the swept volume of the piston.

A. Correct
B. Incorrect
Answer» C.
31.

In a four stroke cycle petrol engine, , the compression

A. starts at 40 after bottom dead centre and ends at 30 before top dead centre
B. starts at 40 before bottom dead centre and ends at 30 after bottom dead centre
C. starts at bottom dead centre and ends at top dead centre
D. may start and end anywhere
Answer» B. starts at 40 before bottom dead centre and ends at 30 after bottom dead centre
32.

In a gas turbine, air is obtained from the atmosphere and compressed in an air compressor.

A. True
B. False
Answer» B. False
33.

The overall efficiency is defined as the ratio of the work obtained at the crankshaft in a given time to the energy supplied during the same time.

A. True
B. False
Answer» B. False
34.

The reflectivity of a reflector is defined as the fraction of neutrons entering the reflector which are returned to the core.

A. Agree
B. Disagree
Answer» B. Disagree
35.

Reflector in nuclear power plants is used to reflect neutrons back into the active core.

A. True
B. False
Answer» B. False
36.

The method of determination of indicated power of a multi cylinder spark ignition engine is by the use of

A. Morse test
B. prony brake test
C. motoring test
D. heat balance test
Answer» B. prony brake test
37.

The turbine of the turbo-prop engine is __________ that of the turbo-jet engine.

A. same as
B. smaller than
C. bigger than
Answer» D.
38.

The pressure at the end of compression, in petrol engines, is approximately

A. 10 bar
B. 20 bar
C. 25 bar
D. 35 bar
Answer» B. 20 bar
39.

The sparking in a petrol engine increases pressure and temperature of the products of combustion, but the volume remains constant.

A. Yes
B. No
Answer» B. No
40.

A higher compression ratio causes

A. pre-ignition
B. increase in detonation
C. an acceleration in the rate of combustion
D. any one of these
Answer» E.
41.

A diesel engine is __________ as compared to petrol engine, both running at rated load.

A. equally efficient
B. less efficient
C. more efficient
Answer» D.
42.

In a four stroke cycle petrol engine, the pressure inside the engine cylinder during the suction stroke is __________ the atmospheric pressure.

A. equal to
B. below
C. above
Answer» C. above
43.

The combustion in compression ignition engines is

A. homogeneous
B. hetrogeneous
C. both (a) and (b)
D. none of these
Answer» C. both (a) and (b)
44.

Which of the following fuel detonates readily ?

A. Benzene
B. Iso-octane
C. Normal heptane
D. Alcohol
Answer» D. Alcohol
45.

The inlet valve of a four stroke cycle internal combustion engine remains open for

A. 130
B. 180
C. 230
D. 270
Answer» D. 270
46.

The cetane (C16H34) which is a straight chain paraffin is assigned a cetane number of

A. 0
B. 50
C. 100
D. 120
Answer» D. 120
47.

Morse test is used to determine the I.P. of a

A. single cylinder petrol engine
B. four stroke engine
C. single cylinder diesel engine
D. multi-cylinder engine
Answer» E.
48.

The increase of efficiency of a compression ignition engine, as the load decreases, is due to

A. higher maximum temperature
B. qualitative governing
C. quantitative governing
D. hit and miss governing
Answer» C. quantitative governing
49.

In order to mix air and petrol in the required proportion and to supply it to the engine during suction stroke, then __________ is employed.

A. fuel pump
B. injector
C. carburettor
D. none of these
Answer» D. none of these
50.

The colour of exhaust from diesel engine is generally

A. white
B. bluish
C. black
D. violent
Answer» D. violent