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This section includes 4791 Mcqs, each offering curated multiple-choice questions to sharpen your Engineering knowledge and support exam preparation. Choose a topic below to get started.
| 4401. |
A nuclear power plant differs from a conventional steam power station only in the steam generating part. |
| A. | Agree |
| B. | Disagree |
| Answer» B. Disagree | |
| 4402. |
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 | |
| 4403. |
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 | |
| 4404. |
The efficiency of roots blower __________ with the increase in pressure ratio. |
| A. | decreases |
| B. | increases |
| C. | does not change |
| Answer» B. increases | |
| 4405. |
The operation of lifts, rams and pumps make use of compressed air. |
| A. | Yes |
| B. | No |
| Answer» B. No | |
| 4406. |
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. | |
| 4407. |
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. | |
| 4408. |
In reciprocating air compressors, isothermal efficiency is used for all sorts of calculations. |
| A. | Correct |
| B. | Incorrect |
| Answer» B. Incorrect | |
| 4409. |
Euler's equation can be used for |
| A. | radial flow compressors |
| B. | axial flow compressors |
| C. | pumps |
| D. | all of these |
| Answer» E. | |
| 4410. |
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 | |
| 4411. |
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 | |
| 4412. |
Free air is the air at atmospheric conditions at any specific location. |
| A. | True |
| B. | False |
| Answer» B. False | |
| 4413. |
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 | |
| 4414. |
A gas turbine used in air-craft should have low weight and small frontal area. |
| A. | Correct |
| B. | Incorrect |
| Answer» B. Incorrect | |
| 4415. |
A closed cycle gas turbine works on |
| A. | Carnot cycle |
| B. | Rankine cycle |
| C. | Ericsson cycle |
| D. | Joule cycle |
| Answer» E. | |
| 4416. |
Air motors work on the cycle which is the reverse of the reciprocating air compressor cycle. |
| A. | Agree |
| B. | Disagree |
| Answer» B. Disagree | |
| 4417. |
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 | |
| 4418. |
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. | |
| 4419. |
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 | |
| 4420. |
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 | |
| 4421. |
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 | |
| 4422. |
A closed cycle gas turbine consists of a |
| A. | compressor |
| B. | heating chamber |
| C. | cooling chamber |
| D. | all of these |
| Answer» E. | |
| 4423. |
A receiver in compressor installations is used to damp pressure waves in compressor discharge. |
| A. | Yes |
| B. | No |
| Answer» B. No | |
| 4424. |
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 | |
| 4425. |
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. | |
| 4426. |
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. | |
| 4427. |
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 | |
| 4428. |
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. | |
| 4429. |
A two stroke cycle engine occupies larger floor area than a four stroke cycle engine. |
| A. | Yes |
| B. | No |
| Answer» C. | |
| 4430. |
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. | |
| 4431. |
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 | |
| 4432. |
In a gas turbine, air is obtained from the atmosphere and compressed in an air compressor. |
| A. | True |
| B. | False |
| Answer» B. False | |
| 4433. |
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 | |
| 4434. |
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 | |
| 4435. |
Reflector in nuclear power plants is used to reflect neutrons back into the active core. |
| A. | True |
| B. | False |
| Answer» B. False | |
| 4436. |
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 | |
| 4437. |
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. | |
| 4438. |
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 | |
| 4439. |
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 | |
| 4440. |
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. | |
| 4441. |
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. | |
| 4442. |
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 | |
| 4443. |
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) | |
| 4444. |
Which of the following fuel detonates readily ? |
| A. | Benzene |
| B. | Iso-octane |
| C. | Normal heptane |
| D. | Alcohol |
| Answer» D. Alcohol | |
| 4445. |
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 | |
| 4446. |
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 | |
| 4447. |
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. | |
| 4448. |
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 | |
| 4449. |
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 | |
| 4450. |
The colour of exhaust from diesel engine is generally |
| A. | white |
| B. | bluish |
| C. | black |
| D. | violent |
| Answer» D. violent | |