Gujarat Technological UniversitySummer 2026 examination

GTU 2151903 Fluid Power Engineering Summer 2026 Question Paper & PDF

B.E. · Mechanical Engineering · Semester 5 · Subject code 2151903
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Total
70 marks
To pass
23 marks (33%)
Duration
2.5 Hours 2:30 PM – 5:00 PM
Questions
5 with internal choice
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Q.1

14 Marks
(a)
3 marks

List any six critical factors that must be considered while selecting a site for a hydropower plant.

(b)
4 marks

Classify hydropower plants based on the operating head of water. Briefly explain the characteristic features of a low-head power plant.

(c)
7 marks

Derive an expression for the force exerted, work done, and efficiency of a jet striking a series of moving curved vanes mounted on the periphery of a wheel. Prove that the maximum efficiency is 50 % for a series of flat vanes.

Q.2

14 Marks
(a)
3 marks
Briefly explain the fundamental concept of jet propulsion in ships.
(b)
4 marks

State four major advantages and four disadvantages of a hydropower plant in the context of power generation.

(c)
7 marks

A jet of water of diameter 50 mm, having a velocity of 25 m/s strikes a single curved vane which is moving with a velocity of 10 m/s in the exact direction of the jet. The jet strikes the vane symmetrically at the center and is deflected through an angle of 120°. Calculate:

iThe force exerted by the jet on the vane in the direction of motion.
iiThe work done per second by the jet on the vane.
iiiThe resultant force exerted on the vane.
(c)
7 marks

A Pelton wheel is to be designed for the following specifications: Shaft power = 11,772 kW; Net head = 380 m; Speed = 750 rpm; Overall efficiency = 86 %. The jet ratio is not to exceed 6. Assuming the coefficient of velocity Cv = 0.985 and the speed ratio Ku = 0.45, determine:

iThe diameter of the wheel
iiThe diameter of the jet
iiiThe number of jets required.

Q.3

14 Marks
(a)
3 marks

Briefly explain why the governing of hydraulic turbines is necessary and name the governing mechanism typically used for a Pelton wheel.

(b)
4 marks

Briefly explain the primary function of a draft tube in a reaction turbine. Why is it not used in an impulse turbine?

(c)
7 marks

A Kaplan turbine runner is to be designed to develop 9100 kW of shaft power. The net available head is 5.6 m. The speed ratio is 2.09 and the flow ratio is 0.68. The overall efficiency is 86 % and the diameter of the boss is one-third the diameter of the runner. Calculate:

iThe diameter of the runner
iiThe specific speed of the turbine.
iiiThe speed of the turbine in rpm.
(a)
3 marks
Explain the fundamental working principle of a Kaplan turbine.
(b)
4 marks

Define a centrifugal pump. Classify centrifugal pumps based on the type of casing and the working head.

(c)
7 marks

A single-acting reciprocating pump has a plunger diameter of 250 mm and a stroke length of 350 mm. The speed of the pump is 60 rpm and it delivers 16.5 liters/s of water. The suction and delivery heads are 3.5 m and 20 m respectively. Find:

iThe theoretical discharge and the coefficient of discharge.
iiThe percentage slip of the pump.
iiiThe theoretical power required to drive the pump.

Q.4

14 Marks
(a)
3 marks

List the essential components of a reciprocating pump and state the primary function of an air vessel.

(b)
4 marks

What is meant by the 'priming' of a centrifugal pump? State why it is an essential step before starting the pump.

(c)
7 marks
Derive an expression for the specific speed of a pump.
(a)
3 marks

Clearly differentiate between the phenomena of 'Surging' and 'Choking' in a centrifugal compressor.

(b)
4 marks

Enlist the essential components of a centrifugal compressor and briefly state the function of each.

(c)
7 marks

Draw the inlet and outlet velocity vector diagrams for the impeller of a centrifugal compressor featuring radial vanes. Apply the principle of angular momentum to derive the expression for the theoretical head (Euler's head) developed by the compressor. Briefly explain how the 'slip factor' modifies this ideal theoretical head.

Q.5

14 Marks
(a)
3 marks

Define the aerodynamic terms 'Lift' and 'Drag' with respect to the aerofoil blading used in an axial flow compressor.

(b)
4 marks
Differentiate between a fluid coupling and a fluid torque converter.
(c)
7 marks

A two-stage reciprocating air compressor operates between suction pressure P1 and delivery pressure P3. Derive the mathematical condition required to achieve minimum work input per cycle, assuming complete and perfect intercooling. Prove that under this condition, the intermediate pressure is the geometric mean of the suction and delivery pressures [P2 = √(P1 x P3)].

(a)
3 marks

Explain the working principle of a hydraulic ram with the help of a neat, labeled sketch.

(b)
4 marks

Describe the mechanism by which a hydraulic intensifier increases the pressure intensity of a fluid from a low-pressure source.

(c)
7 marks

What is the primary function of a hydraulic accumulator in a fluid power system? Draw a neat sketch of a weight-loaded hydraulic accumulator, explain its working mechanism, and state its practical applications.

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About this paper

Official Gujarat Technological University (GTU) examination paper for Fluid Power Engineering (Summer 2026, B.E. · Mechanical Engineering, Sem 5). Features complete 70-mark regular & remedial examination pattern, official marking distribution across all 5 questions, and direct 1-click official PDF download.

Transcribed for student exam preparation from Gujarat Technological University official examination archives. Questions, syllabus guidelines, and curriculum marking schemes remain the intellectual property of Gujarat Technological University.

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