JAWAHARLAL NEHRU TECHNOLOGICAL UNIVERSITY HYDERABAD

JAWAHARLAL NEHRU TECHNOLOGICAL UNIVERSITY HYDERABAD B.Tech IV Year VIBRATION AND AERO-ELASTICITY Previous Question Paper (February/March - 2022 - R18)

B.Tech | IV Year | I Semester | R18 | February/March - 2022

Answer PaperPaper Code: 157ECMaximum Marks: 75Time: 3 Hours

Answer any Five Questions. All Questions Carry Equal Marks.

Main

1

Two helical springs, one made of steel and the other made of aluminum, have identical values of wire diameter d and mean coil diameter D.

15 marks
a

If the number of turns in the steel spring is 10, determine the number of turns required in the aluminum spring whose weight will be same as that of the steel spring.

8 marks

Answer

The weight of a helical spring is given by the product of the volume of the wire and the density of the material, W = ρ × V. The volume of the wire is V = (π × d2 / 4) × (π × D × n), where d is the wire diameter, D is the mean coil diameter, and n is the number of turns. Since the wire diameter d and mean coil diameter D are identical for both springs, the volume is directly proportional to the number of turns n. Given the weights are equal, ρs × ns = ρa × na, where the subscripts s and a denote steel and aluminum respectively. Taking standard densities of ρs ≈ 7850 kg/m3 and ρa ≈ 2700 kg/m3, and ns = 10, the number of turns for the aluminum spring is na = (ρs / ρa) × ns = (7850 / 2700) × 10 ≈ 29.07 turns.

b

Find the spring constants of the two springs.

7 marks

Answer

The spring constant k of a helical spring is defined by the formula:

k = (G × d4) / (8 × D3 × n)

where G is the shear modulus of the material. For steel, Gs ≈ 80 GPa, and for aluminum, Ga ≈ 26 GPa. The ratio of the spring constants is:

ks / ka = (Gs / Ga) × (na / ns)

Substituting the values Gs = 80, Ga = 26, ns = 10, and na = 29.07:

ks / ka = (80 / 26) × (29.07 / 10) ≈ 3.0769 × 2.907 ≈ 8.945

Thus, the steel spring is approximately 8.945 times stiffer than the aluminum spring for the given dimensions.

2

An electronic instrument, weighing 200 N, is supported on a rubber mounting whose force deflection relationship is given by

F(x) = 800 x + 40 x3

where the force (F) and the deflection (x) are in N and mm, respectively. Determine the following:

15 marks
a

Equivalent linear spring constant of the mounting at its static equilibrium position.

8 marks

Answer

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b

Deflection of the mounting corresponding to the equivalent linear spring constant.

7 marks

Answer

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315 marks
a

A spring-mass system has a natural frequency of 10 Hz. When the spring constant is reduced by 800 N/m, the frequency is altered by 45 percent. Find the mass and spring constant of the original system.

8 marks

Answer

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b

A simple pendulum is set into oscillation from its rest position by giving it an angular velocity of 1 rad/s. It is found to oscillate with an amplitude of 0.5 rad. Find the natural frequency and length of the pendulum.

7 marks

Answer

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415 marks
a

A simple pendulum is found to vibrate at a frequency of 0.5 Hz in a vacuum and 0.45 Hz in a viscous fluid medium. Find the damping constant, assuming the mass of the bob of the pendulum is 1 kg.

8 marks

Answer

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b

Derive an expression for the time at which the response of a critically damped system will attain its maximum value. Also find the expression for the maximum response.

7 marks

Answer

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5

Solve the problem for a multi-degree of freedom system with m1 = 10 kg, m2 = 15 kg and k = 320 N/m.

15 marks

Answer

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6

The mass and stiffness matrices and the mode shapes of a two-degree-of-freedom system are given. If the first natural frequency is given by

ω1 = 1.4142
, determine the masses m1 and m2 and the second natural frequency of vibration, ω2.

15 marks

Answer

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7

Using Rayleigh's method, determine the first natural frequency of vibration of a system with springs k1 = k, k2 = 2k, k3 = 3k, k4 = k and masses m1 = m, m2 = 2m, m3 = 3m.

15 marks

Answer

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8

Obtain the expression for the divergence speed of a two-dimensional wing.

15 marks

Answer

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About this paper

This page contains the question paper of VIBRATION AND AERO-ELASTICITY from JAWAHARLAL NEHRU TECHNOLOGICAL UNIVERSITY HYDERABAD for B.Tech AE IV Year I Semester, February/March - 2022, R18.

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