JAWAHARLAL NEHRU TECHNOLOGICAL UNIVERSITY HYDERABAD
JAWAHARLAL NEHRU TECHNOLOGICAL UNIVERSITY HYDERABAD B.Tech II MECHANICS OF FLUIDS Previous Question Paper (April - 2018 - R13)
Note: This question paper contains two parts A and B. Part A is compulsory which carries 25 marks. Answer all questions in Part A. Part B consists of 5 Units. Answer any one full question from each unit. Each question carries 10 marks and may have a, b, c as sub questions.
PART-A
State Pascal’s law.
Answer
Pascal's law states that the pressure at any point in a fluid at rest is the same in all directions.
Define Archimedes’s principle. Give an example.
Answer
Archimedes's principle states that a body immersed in a fluid is buoyed up by a force equal to the weight of the fluid displaced by the body. An example is a ship floating on water, where the weight of the water displaced by the hull equals the total weight of the ship.
Differentiate between stream line and streak line.
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What is vorticity?
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State Bernoulli’s equation.
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State momentum equation.
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What is Pressure drag?
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Define the term boundary layer thickness.
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What is Moody’s chart?
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State Darcy’s equation.
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PART-B
What is Surface tension and capillary effect? How are they affected?
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The absolute pressure in water at a depth of 5 m is read to be 145 kPa. Determine (i) the local atmospheric pressure, and (ii) The absolute pressure at a depth of 5 m in a liquid whose specific gravity is 0.78 at the same location.
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Differentiate between U-tube differential manometers and inverted U-tube differential manometers. Where are they used?
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Calculate the pressure and density of air at a height of 4000 m from sea-level where pressure and temperature of air are 10.143 N/cm2 and 15ºC respectively. The temperature lapse rate is given as 0.0065ºC/m. Take density of air at sea-level equal to 1.285 kg/m3.
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Define the following and give one practical example for each: (i) Unsteady flow (ii) Uniform flow (iii) Turbulent flow (iv) Three dimensional flow.
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Derive equation of continuity for one dimensional flow for an incompressible flow.
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Derive equation of continuity for a compressible flow and show that it tends to divergence of velocity equal to zero for incompressible fluids. State clearly the assumptions made.
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For the velocity potential function, φ = x2 – y2, find the velocity components in x and y direction. Also show that φ represents a possible case of fluid flow.
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Derive the Euler’s equation and from this obtain the Bernoulli’s equation for the incompressible flow.
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Define Reynolds’s number and Froude’s number. Derive the expressions for the two numbers.
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What is meant by geometric, kinematic and dynamic similarities? Are these similarities truly attainable? If not why?
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How will you determine total drag of a ship or partially submerged ship?
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Explain the development of boundary layer along a flat plate held parallel to uniform flow. Point out salient features.
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Write a brief note on Prandtl’s boundary layer theory.
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How does the ratio of displacement thickness to boundary layer thickness (δ*/δ) for a laminar boundary layer compare with that for a turbulent boundary layer? Determine a qualitative answer from inspection of the velocity profiles within the boundary layers.
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What are the different methods to prevent the separation of boundary layer? Explain.
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Discuss various minor losses involved in a pipe flow system.
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How will you determine the loss of head due to friction in pipes by using Darcy’s formula?
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Differentiate between major and minor losses. Why the minor losses in a parallel pipes flow are neglected.
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Differentiate between flow between parallel plates and flow through long tubes.
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