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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.
4501. |
If the compression ratio in I.C. engine increases, then its thermal efficiency will |
A. | decrease |
B. | increase |
C. | remain same |
Answer» C. remain same | |
4502. |
In a Kaplan turbine runner, the number of blades are generally between |
A. | 2 to 4 |
B. | 4 to 8 |
C. | 8 to l6 |
D. | 16 to 24 |
Answer» C. 8 to l6 | |
4503. |
A Pelton wheel develops 1750 kW under a head of 100 metres while running at 200 r.p.m. and discharging 2500 litres of water per second. The unit power of the wheel is |
A. | 0.25 kW |
B. | 0.75 kW |
C. | 1.75 kW |
D. | 3.75 kW |
Answer» D. 3.75 kW | |
4504. |
Geometric similarity is said to exist between the model and the prototype, if both of them |
A. | have identical velocities |
B. | are equal in size and shape |
C. | are identical in shape, but differ only in size |
D. | have identical forces |
Answer» D. have identical forces | |
4505. |
Which of the following turbine is preferred for 0 to 25 m head of water? |
A. | Pelton wheel |
B. | Kaplan turbine |
C. | Francis turbine |
D. | none of these |
Answer» C. Francis turbine | |
4506. |
When the speed of the pump increases, its net positive suction head (NPSH) requirement decreases. |
A. | Agree |
B. | Disagree |
Answer» C. | |
4507. |
The specific speed from 160 to 500 r.p.m. of a centrifugal pump indicates that the pump is |
A. | slow speed with radial flow at outlet |
B. | medium speed with radial flow at outlet |
C. | high speed with radial flow at outlet |
D. | high speed with axial flow at outlet |
Answer» E. | |
4508. |
In an impulse turbine, the jet of water impinges on the bucket with a low velocity and after flowing over the vanes, leaves with a high velocity. |
A. | True |
B. | False |
Answer» C. | |
4509. |
The ratio of quantity of liquid discharged per second from the pump to the quantity of liquid passing per second through the impeller is known as |
A. | manometric efficiency |
B. | mechanical efficiency |
C. | overall efficiency |
D. | volumetric efficiency |
Answer» E. | |
4510. |
Overall efficiency of a centrifugal pump is the ratio of |
A. | energy available at the impeller to the energy supplied to the pump by the prime mover |
B. | actual workdone by the pump to the energy supplied to the pump by the prime mover |
C. | energy supplied to the pump to the energy available at the impeller |
D. | manometric head to the energy supplied by the impeller per kN of water |
Answer» C. energy supplied to the pump to the energy available at the impeller | |
4511. |
A hydraulic intensifier is a device used to increase the intensity of pressure of water by means of energy available from a large quantity of water at a low pressure. |
A. | Correct |
B. | Incorrect |
Answer» B. Incorrect | |
4512. |
The discharge through a reaction turbine __________ with the increase in unit speed. |
A. | remains same |
B. | increases |
C. | decreases |
Answer» D. | |
4513. |
The depth of the bucket for a Pelton wheel is generally __________ the diameter of jet. |
A. | equal to |
B. | 1.2 times |
C. | 1.8 times |
D. | double |
Answer» C. 1.8 times | |
4514. |
An impulse turbine is used for |
A. | low head of water |
B. | high head of water |
C. | medium head of water |
D. | high discharge |
Answer» C. medium head of water | |
4515. |
In a mixed flow centrifugal pump, the flow through the impeller is a combination of radial and axial flows. |
A. | Correct |
B. | Incorrect |
Answer» B. Incorrect | |
4516. |
Which of the following pump is sucessfully used for lifting water to the boilers? |
A. | Centrifugal pump |
B. | Reciprocating pump |
C. | Jet pump |
D. | Air-lift pump |
Answer» D. Air-lift pump | |
4517. |
When the nozzle operates with the maximum mass flow, the nozzle is said to be |
A. | choked |
B. | underdamping |
C. | overdamping |
D. | none of these |
Answer» B. underdamping | |
4518. |
In order to reduce the rotor speed of an impulse turbine, the method employed is |
A. | velocity compounding |
B. | pressure compounding |
C. | pressure-velocity compounding |
D. | all of these |
Answer» E. | |
4519. |
The nozzle efficiency is the ratio of |
A. | workdone on the blades to the energy supplied to the blades |
B. | workdone on the blades per kg of steam to the total energy supplied per stage per kg of steam |
C. | energy supplied to the blades per kg of steam to the total energy supplied per stage per kg of steam |
D. | none of the above |
Answer» D. none of the above | |
4520. |
The friction in the nozzle __________ exit velocity of steam. |
A. | has no effect on |
B. | decreases |
C. | increases |
Answer» C. increases | |
4521. |
A stage, in reaction turbine, is represented by |
A. | number of casing |
B. | number of entries of steam |
C. | number of exits of steam |
D. | each row of blades |
Answer» E. | |
4522. |
The ratio of the workdone on the blades per kg of steam to the total energy supplied per stage per kg of steam is called |
A. | blading efficiency |
B. | nozzle efficiency |
C. | stage efficiency |
D. | mechanical efficiency |
Answer» D. mechanical efficiency | |
4523. |
The diagram efficiency is the ratio of |
A. | workdone on the blades to the energy supplied to the blades |
B. | workdone on the blades per kg of steam to the total energy supplied per stage per kg of steam |
C. | energy supplied to the blades per kg of steam to the total energy supplied per stage per kg of steam |
D. | none of the above |
Answer» B. workdone on the blades per kg of steam to the total energy supplied per stage per kg of steam | |
4524. |
The Rankine efficiency depends upon total useful heat drop and total isentropic heat drop. |
A. | Correct |
B. | Incorrect |
Answer» C. | |
4525. |
Blading efficiency is also known as |
A. | stage efficiency |
B. | diagram efficiency |
C. | nozzle efficiency |
D. | none of these |
Answer» C. nozzle efficiency | |
4526. |
The reheat factor depends upon |
A. | initial pressure and superheat |
B. | exit pressure |
C. | turbine stage efficiency |
D. | all of these |
Answer» E. | |
4527. |
A nozzle is said to be a divergent nozzle |
A. | when the cross-section of the nozzle increases continuously from entrance to exit |
B. | when the cross-section of the nozzle decreases continuously from entrance to exit |
C. | when the cross-section of the nozzle first decreases from entrance to throat and then increases from its throat to exit |
D. | none of the above |
Answer» B. when the cross-section of the nozzle decreases continuously from entrance to exit | |
4528. |
The ratio of the cumulative heat drop to the isentropic heat drop is called reheat factor. |
A. | Yes |
B. | No |
Answer» B. No | |
4529. |
The compounding of turbines is done in order to |
A. | reduce speed of rotor |
B. | improve efficiency |
C. | reduce exit losses |
D. | all of these |
Answer» E. | |
4530. |
The pressure of steam, in reaction turbines, is reduced in the fixed blades as well as in moving blades. |
A. | Correct |
B. | Incorrect |
Answer» B. Incorrect | |
4531. |
When the cross-section of a nozzle first increases from its entrance to throat, and then decreases from its throat to exit, it is not a convergent-divergent nozzle. |
A. | Yes |
B. | No |
Answer» B. No | |
4532. |
The purpose of governing in steam turbines is to |
A. | maintain the speed of the turbine |
B. | reduce the effective heat drop |
C. | reheat the steam and improve its quality |
D. | completely balance against end thrust |
Answer» B. reduce the effective heat drop | |
4533. |
De-Laval turbines are mostly used |
A. | where low speeds are required |
B. | for small power purposes and low speeds |
C. | for large power purposes |
D. | for small power purposes and high speeds |
Answer» E. | |
4534. |
The efficiency ratio is the ratio of total useful heat drop to the total isentropic heat drop. |
A. | Agree |
B. | Disagree |
Answer» B. Disagree | |
4535. |
The velocity of steam, in reaction turbines, is increased in the fixed blades as well as in moving blades. |
A. | True |
B. | False |
Answer» B. False | |
4536. |
The critical pressure ratio for gases is |
A. | 0.528 |
B. | 0.546 |
C. | 0.577 |
D. | 0.582 |
Answer» B. 0.546 | |
4537. |
The efficiency of a pressure-velocity compounded impulse turbine is __________ as compared to pressure compounded impulse turbine. |
A. | same |
B. | less |
C. | more |
Answer» C. more | |
4538. |
The effect of supersaturation is that the |
A. | mass of the steam discharged increases |
B. | entropy and specific volume of the steam increases |
C. | exit velocity of steam reduces |
D. | all of these |
Answer» E. | |
4539. |
A single stage turbine is not used because it requires large reduction gearing due to very high rotational speed. |
A. | Agree |
B. | Disagree |
Answer» B. Disagree | |
4540. |
In an impulse reaction turbine, the pressure drops gradually and continuously over |
A. | fixed blades |
B. | moving blades |
C. | both fixed and moving blades |
D. | none of these |
Answer» D. none of these | |
4541. |
When the inlet pressure of steam is equal to the exit pressure, then |
A. | there is a pressure drop in the nozzle |
B. | fluid flows through the nozzle |
C. | pressure drops and fluid flows through the nozzle |
D. | there is no pressure drop and fluid does not flow through the nozzle |
Answer» E. | |
4542. |
In velocity compounding of an impulse turbine, the expansion of steam takes place in a nozzle or a set of nozzles from the boiler pressure to condenser pressure. |
A. | True |
B. | False |
Answer» B. False | |
4543. |
The effect of friction on the flow of steam through a nozzle is to |
A. | decrease the mass flow rate and to increase the wetness of steam |
B. | increase the mass flow rate and to increase the exit temperature |
C. | decrease the mass flow rate and to decrease the wetness of steam |
D. | increase the exit temperature without any effect on mass flow rate |
Answer» D. increase the exit temperature without any effect on mass flow rate | |
4544. |
In pressure compounding of an impulse turbine, the total pressure drop of the steam does not take place in the first nozzle ring, but is divided equally among all the nozzle rings. |
A. | Agree |
B. | Disagree |
Answer» B. Disagree | |
4545. |
In an ideal impulse turbine, the |
A. | absolute velocity at the inlet of moving blade is equal to that at the outlet |
B. | relative velocity at the inlet of the moving blade is equal to that at the outlet |
C. | axial velocity at inlet is equal to that at the outlet |
D. | whirl velocity at inlet is equalto that at the outlet |
Answer» C. axial velocity at inlet is equal to that at the outlet | |
4546. |
During flow through a nozzle, no heat is supplied or rejected by the steam. |
A. | Agree |
B. | Disagree |
Answer» B. Disagree | |
4547. |
In a reaction turbine when the degree of reaction is zero, then there is |
A. | no heat drop in moving blades |
B. | no heat drop in fixed blades |
C. | maximum heat drop in moving blades |
D. | maximum heat drop in fixed blades |
Answer» B. no heat drop in fixed blades | |
4548. |
The pressure compounded impulse turbine as compared to velocity compounded turbine require __________ number of stages. |
A. | same |
B. | less |
C. | more |
Answer» D. | |
4549. |
In a single stage impulse turbine, the velocity of steam approaching nozzles is negligible. |
A. | True |
B. | False |
Answer» B. False | |
4550. |
The impulse turbine rotor efficiency will have a maximum value of 0.5 cos2 , where is the nozzle exit flow angle, if the |
A. | blades are equiangular |
B. | blade velocity coefficient is unity |
C. | blades are equiangular and frictionless |
D. | blade solidity is 0.65 |
Answer» D. blade solidity is 0.65 | |