JAWAHARLAL NEHRU TECHNOLOGICAL UNIVERSITY HYDERABAD

JAWAHARLAL NEHRU TECHNOLOGICAL UNIVERSITY HYDERABAD B.Tech II FLUID MECHANICS AND HEAT TRANSFER Previous Question Paper (February - 2024 - R16)

B.Tech | II | II | R16 | February - 2024

Answer PaperPaper Code: 134BBMaximum Marks: 75Time: 3 hours

Answer any five questions.

Question paper consists of Part A and Part B. Part A is compulsory. In Part B, Answer any one question from each unit.

Part A

Answer all questions.

125 marks
a

Define Pascal’s law.

2 marks

Answer

Pascal’s law states that the pressure at any point in a static fluid is equal in all directions. Furthermore, any change in pressure applied to an enclosed fluid is transmitted undiminished to every portion of the fluid and to the walls of the container.

b

State the conditions for rotational and irrotational flow.

3 marks

Answer

A flow is considered rotational if the fluid particles rotate about their own axes while moving along a streamline, which occurs when the vorticity vector is non-zero (ω ≠ 0). A flow is irrotational if the fluid particles do not rotate about their own axes, occurring when the vorticity vector is zero (ω = 0), implying the velocity field is the gradient of a scalar potential.

c

Define vena contracta. State its significance.

2 marks

Answer

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d

What do you mean by the coefficient of discharge?

3 marks

Answer

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e

What do you mean by thermal diffusivity?

2 marks

Answer

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f

State Fourier’s law of conduction.

3 marks

Answer

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g

Define convection heat transfer.

2 marks

Answer

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h

Differentiate free and forced convection.

3 marks

Answer

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i

Define grey body. Give examples.

2 marks

Answer

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j

Show the temperature trend in a counterflow heat exchanger.

3 marks

Answer

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Part B

210 marks
a

Classify the types of fluid flows.

5 marks

Answer

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b

The velocity distribution in a viscous flow over a plate is given by

u = 4y - y2
. Where u is the velocity at distance y from the plate. If the coefficient of dynamic viscosity is 1.5 Pa.sec, determine the shear stress at y=0 and y = 2.

5 marks

Answer

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OR
310 marks
a

Explain stream and velocity potential functions.

5 marks

Answer

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b

In a flow field, the velocity components as defined as follows.

U = x2 + y2 + z2, v = yz2 + xy, w = -3xz - 2xyz + z3/3
. Determine whether the flow is steady or not.

5 marks

Answer

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410 marks
a

Derive the expression for the rate of flow of fluid through an orifice meter.

5 marks

Answer

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b

A 20 cm × 10 cm venturimeter is provided by a vertical pipeline carrying oil of a specific gravity of 0.85. The difference in elevation of the throat section and entrance section of the venturimeter is 0.5 m. The differential U-tube Venturimeter shows a gauge difference of 40 cm. The specific gravity of mercury is 13.6. Calculate the discharge of oil in litres per sec. Take Cd = 0.98.

5 marks

Answer

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OR
510 marks
a

Derive Bernoulli's equation from Euler's equation.

5 marks

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b

Discuss the following: i) Body forces, ii) Surface forces.

5 marks

Answer

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610 marks
a

Derive an expression for a generalized heat conduction equation in a Cartesian coordinate system.

5 marks

Answer

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b

A 30 cm thick wall of the reactor is made up of an inner layer of firebrick

k1 = 0.85 W/mK
covered with a layer of insulation
k2 = 0.15 W/mK
. The reactor operates at a temperature of 1600 K while the ambient temperature is 295 K. Calculate the thickness of the firebrick and insulation which gives a minimum heat loss presuming that the insulating material has a maximum temperature of 1475 K.

5 marks

Answer

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OR
710 marks
a

Define thermal conductivity and how it can be measured. Differentiate between thermal conductivity and thermal conductance.

5 marks

Answer

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b

A stainless steel tube (

ks = 19 W/mK
) of 2 cm ID and 5 cm OD is insulated with 3 cm thick asbestos (
ka = 0.2 W/mK
). If the temperature difference between the innermost and outermost surfaces is 600 °C. Determine the heat transfer rate per unit length.

5 marks

Answer

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810 marks
a

Explain Rayleigh's method of dimensional analysis.

5 marks

Answer

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b

A glazed window made of 8 mm thick glass of thermal conductivity 1.5 W/m K as its outside surface maintained at 50 °C so that frosting is reduced. The surrounding is at -10 °C with a convective coefficient of 55 W/m2K. The desired condition is attained by providing uniform heat flux at the inner surface of the window which is fitted into a room where the air temperature is 25 °C with a convection coefficient of 12.5 W/m2 K. Calculate the heat required per m2 area.

5 marks

Answer

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OR
910 marks
a

Explain the lift and drag phenomenon.

5 marks

Answer

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b

Engine oil at 60 °C flows over a 5 m long flat plate whose temperature is 20 °C with a velocity of 2 m/s. Determine the total drag force and the rate of heat transfer per unit width of the entire plate.

5 marks

Answer

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1010 marks
a

Explain the applications of radiation shields in heat transfer.

5 marks

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b

A black body of 0.2 m2 area has an effective temperature of 800 K. Calculate the total rate of energy emission, the intensity of normal radiation, the intensity of radiation along a direction 60° to the normal and the wavelength of maximum monochromatic emissive power.

5 marks

Answer

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OR
1110 marks
a

Explain the fouling factor and its influence on the heat exchangers.

5 marks

Answer

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b

A furnace is approximated as an equilateral triangular duct of sufficient length so that end effects can be neglected. The hot wall of the furnace is maintained at a temperature of 900 K and has an emissivity of 0.8. The cold wall is at 400 K and has the same emissivity. Find the net radiation heat flux leaving the wall. The third wall of the furnace may be assumed as a reradiating surface.

5 marks

Answer

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About this paper

This page contains the question paper of FLUID MECHANICS AND HEAT TRANSFER from JAWAHARLAL NEHRU TECHNOLOGICAL UNIVERSITY HYDERABAD for B.Tech MECT-MCT-MEM II II, February - 2024, R16.

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