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7/28/2019 a107412101-Vibrations and Structural Dynamics_2nd Mid
1/8
Code No: A107412101 Set No. 1JAWAHARLAL NEHRU TECHNOLOGICAL UNIVERSITY HYDERABAD
IV B.Tech. I Sem., II Mid-Term Examinations, November 2010VIBRATIONS AND STRUCTURAL DYNAMICS
Objective ExamName: ______________________________ Hall Ticket No.
Answer All Questions. All Questions Carry Equal Marks.Time: 20 Min. Marks: 20.
I Choose the correct alternative:
1. The influence coefficient of cantilever beam at the free end subjected to point load is given be
[ ]
a) 3L3/EI b) L
3/3EI c) L
3/EI d) 2L
3/3EI
2. The influence coefficient of simply supported beam subjected to point load at the centre is given by
[ ]
a) L3/48EI b) 48L
3/3EI c) L
3/3EI d) 48L
3/EI
3. The influence coefficient of fixed beam subjected to point load at the centre is given by [ ]a) L
3/3EI b) L
3/48EI c) L
3/192EI d) 192L
3/EI
4. Stodola method is [ ]a) An exact method b) Approximate method c) Derived method d) Analytical method
5. When the running speed of the shaft is equal to the critical speed, the amplitude of vibrationbecomes [ ]
a) Finite b) Infinite c) Cannot be determined d) twice the amplitude at half the critical speed
6. If y is the static deflection of shaft, then the angular frequency of vibration is [ ]
a) root of g/y b) root of 2g/y c) root of y/g d) none
7. Whirling speed of the shaft is [ ]a) speed of the shaft below resonance condition b) speed of the shaft above resonance condition
c) speed of the shaft at resonance d) speed of the shaft at half the resonance speed
8. Dunkerleys method considers [ ]
a) Static deflections b) Dynamic deflections
c) both static and dynamic deflections d) neither static nor dynamic deflections
9. The accuracy of solution is good if the problem of dynamic vibrations is solved using [ ]
a) lumped mass modelb) consistent mass matrix methodc) either lumped mass model or mass matrix method
d) neither lumped mass model nor mass matrix method
10. The unit of influence coefficient is [ ]
a) N/m b) m/N c) n/m2
d) none
Cont2
7/28/2019 a107412101-Vibrations and Structural Dynamics_2nd Mid
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Code No: A107412101 :2: Set No. 1
II Fill in the blanks
11. Whirling speed of the shaft also called____________
12. The Dunkerleys formula is ______________
13. The Rayleighs formula for shaft subjected to point loads is ______________
14. Rayleighs formula for transverse vibrations of beam to determine the natural frequency is
____________
15. The governing equation for dynamic vibrations using FEM approach with damping is ___________
16. The total lumped mass matrix for dynamic vibrations using FEM approach is____________
17. A bar of length L is divided into two elements of equal lengths. If A is the area, E, Youngsmodulus, , the density, the total consistent mass matrix is given by_____________
18. Total stiffness matrix for a bar of dimensions and properties L, A, E and is ______________
19. The total lumped mass matrix for a bar of dimensions and properties L, A, E and is___________
20. The vibrations which die down in short duration of time are called___________
-oOo-
7/28/2019 a107412101-Vibrations and Structural Dynamics_2nd Mid
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Code No: A107412101 Set No. 2JAWAHARLAL NEHRU TECHNOLOGICAL UNIVERSITY HYDERABAD
IV B.Tech. I Sem., II Mid-Term Examinations, November 2010VIBRATIONS AND STRUCTURAL DYNAMICS
Objective ExamName: ______________________________ Hall Ticket No.
Answer All Questions. All Questions Carry Equal Marks.Time: 20 Min. Marks: 20.
I Choose the correct alternative:
1. Stodola method is [ ]
a) An exact method b) Approximate method c) Derived method d) Analytical method
2. When the running speed of the shaft is equal to the critical speed, the amplitude of vibration
becomes [ ]
a) Finite b) Infinite c) Cannot be determined d) twice the amplitude at half the critical speed
3. If y is the static deflection of shaft, then the angular frequency of vibration is [ ]
a) root of g/y b) root of 2g/y c) root of y/g d) none
4. Whirling speed of the shaft is [ ]
a) speed of the shaft below resonance condition b) speed of the shaft above resonance conditionc) speed of the shaft at resonance d) speed of the shaft at half the resonance speed
5. Dunkerleys method considers [ ]a) Static deflections b) Dynamic deflections
c) both static and dynamic deflections d) neither static nor dynamic deflections
6. The accuracy of solution is good if the problem of dynamic vibrations is solved using [ ]
a) lumped mass modelb) consistent mass matrix method
c) either lumped mass model or mass matrix methodd) neither lumped mass model nor mass matrix method
7. The unit of influence coefficient is [ ]a) N/m b) m/N c) n/m
2d) none
8. The influence coefficient of cantilever beam at the free end subjected to point load is given be[ ]
a) 3L3/EI b) L
3/3EI c) L
3/EI d) 2L
3/3EI
9. The influence coefficient of simply supported beam subjected to point load at the centre is given by[ ]
a) L3/48EI b) 48L
3/3EI c) L
3/3EI d) 48L
3/EI
10. The influence coefficient of fixed beam subjected to point load at the centre is given by [ ]
a) L3/3EI b) L
3/48EI c) L
3/192EI d) 192L
3/EI
Cont2
7/28/2019 a107412101-Vibrations and Structural Dynamics_2nd Mid
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Code No: A107412101 :2: Set No. 2
II Fill in the blanks
11. Rayleighs formula for transverse vibrations of beam to determine the natural frequency is
____________
12. The governing equation for dynamic vibrations using FEM approach with damping is ___________
13. The total lumped mass matrix for dynamic vibrations using FEM approach is____________
14. A bar of length L is divided into two elements of equal lengths. If A is the area, E, Youngsmodulus, , the density, the total consistent mass matrix is given by_____________
15. Total stiffness matrix for a bar of dimensions and properties L, A, E and is ______________
16. The total lumped mass matrix for a bar of dimensions and properties L, A, E and is___________
17. The vibrations which die down in short duration of time are called___________
18. Whirling speed of the shaft also called____________
19. The Dunkerleys formula is ______________
20. The Rayleighs formula for shaft subjected to point loads is ______________
-oOo-
7/28/2019 a107412101-Vibrations and Structural Dynamics_2nd Mid
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Code No: A107412101 Set No. 3JAWAHARLAL NEHRU TECHNOLOGICAL UNIVERSITY HYDERABAD
IV B.Tech. I Sem., II Mid-Term Examinations, November 2010VIBRATIONS AND STRUCTURAL DYNAMICS
Objective ExamName: ______________________________ Hall Ticket No.
Answer All Questions. All Questions Carry Equal Marks.Time: 20 Min. Marks: 20.
I Choose the correct alternative:
1. If y is the static deflection of shaft, then the angular frequency of vibration is [ ]
a) root of g/y b) root of 2g/y c) root of y/g d) none
2. Whirling speed of the shaft is [ ]
a) speed of the shaft below resonance condition b) speed of the shaft above resonance condition
c) speed of the shaft at resonance d) speed of the shaft at half the resonance speed
3. Dunkerleys method considers [ ]
a) Static deflections b) Dynamic deflectionsc) both static and dynamic deflections d) neither static nor dynamic deflections
4. The accuracy of solution is good if the problem of dynamic vibrations is solved using [ ]a) lumped mass model
b) consistent mass matrix method
c) either lumped mass model or mass matrix methodd) neither lumped mass model nor mass matrix method
5. The unit of influence coefficient is [ ]a) N/m b) m/N c) n/m
2d) none
6. The influence coefficient of cantilever beam at the free end subjected to point load is given be
[ ]a) 3L
3/EI b) L
3/3EI c) L
3/EI d) 2L
3/3EI
7. The influence coefficient of simply supported beam subjected to point load at the centre is given by[ ]
a) L3/48EI b) 48L
3/3EI c) L
3/3EI d) 48L
3/EI
8. The influence coefficient of fixed beam subjected to point load at the centre is given by [ ]
a) L3/3EI b) L
3/48EI c) L
3/192EI d) 192L
3/EI
9. Stodola method is [ ]a) An exact method b) Approximate method c) Derived method d) Analytical method
10. When the running speed of the shaft is equal to the critical speed, the amplitude of vibrationbecomes [ ]
a) Finite b) Infinite c) Cannot be determined d) twice the amplitude at half the critical speed
Cont2
7/28/2019 a107412101-Vibrations and Structural Dynamics_2nd Mid
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Code No: A107412101 :2: Set No. 3
II Fill in the blanks
11. The total lumped mass matrix for dynamic vibrations using FEM approach is____________
12. A bar of length L is divided into two elements of equal lengths. If A is the area, E, Youngs
modulus, , the density, the total consistent mass matrix is given by_____________
13. Total stiffness matrix for a bar of dimensions and properties L, A, E and is ______________
14. The total lumped mass matrix for a bar of dimensions and properties L, A, E and is___________
15. The vibrations which die down in short duration of time are called___________
16. Whirling speed of the shaft also called____________
17. The Dunkerleys formula is ______________
18. The Rayleighs formula for shaft subjected to point loads is ______________
19. Rayleighs formula for transverse vibrations of beam to determine the natural frequency is
____________
20. The governing equation for dynamic vibrations using FEM approach with damping is ___________
-oOo-
7/28/2019 a107412101-Vibrations and Structural Dynamics_2nd Mid
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Code No: A107412101 Set No. 4JAWAHARLAL NEHRU TECHNOLOGICAL UNIVERSITY HYDERABAD
IV B.Tech. I Sem., II Mid-Term Examinations, November 2010VIBRATIONS AND STRUCTURAL DYNAMICS
Objective ExamName: ______________________________ Hall Ticket No.
Answer All Questions. All Questions Carry Equal Marks.Time: 20 Min. Marks: 20.
I Choose the correct alternative:
1. Dunkerleys method considers [ ]
a) Static deflections b) Dynamic deflections
c) both static and dynamic deflections d) neither static nor dynamic deflections
2. The accuracy of solution is good if the problem of dynamic vibrations is solved using [ ]
a) lumped mass model
b) consistent mass matrix methodc) either lumped mass model or mass matrix method
d) neither lumped mass model nor mass matrix method
3. The unit of influence coefficient is [ ]
a) N/m b) m/N c) n/m2
d) none
4. The influence coefficient of cantilever beam at the free end subjected to point load is given be
[ ]a) 3L
3/EI b) L
3/3EI c) L
3/EI d) 2L
3/3EI
5. The influence coefficient of simply supported beam subjected to point load at the centre is given by[ ]
a) L3/48EI b) 48L3/3EI c) L3/3EI d) 48L3/EI
6. The influence coefficient of fixed beam subjected to point load at the centre is given by [ ]a) L
3/3EI b) L
3/48EI c) L
3/192EI d) 192L
3/EI
7. Stodola method is [ ]a) An exact method b) Approximate method c) Derived method d) Analytical method
8. When the running speed of the shaft is equal to the critical speed, the amplitude of vibrationbecomes [ ]
a) Finite b) Infinite c) Cannot be determined d) twice the amplitude at half the critical speed
9. If y is the static deflection of shaft, then the angular frequency of vibration is [ ]a) root of g/y b) root of 2g/y c) root of y/g d) none
10. Whirling speed of the shaft is [ ]a) speed of the shaft below resonance condition b) speed of the shaft above resonance condition
c) speed of the shaft at resonance d) speed of the shaft at half the resonance speed
Cont2
7/28/2019 a107412101-Vibrations and Structural Dynamics_2nd Mid
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Code No: A107412101 :2: Set No. 4
II Fill in the blanks
11. Total stiffness matrix for a bar of dimensions and properties L, A, E and is ______________
12. The total lumped mass matrix for a bar of dimensions and properties L, A, E and is___________
13. The vibrations which die down in short duration of time are called___________
14. Whirling speed of the shaft also called____________
15. The Dunkerleys formula is ______________
16. The Rayleighs formula for shaft subjected to point loads is ______________
17. Rayleighs formula for transverse vibrations of beam to determine the natural frequency is____________
18. The governing equation for dynamic vibrations using FEM approach with damping is ___________
19. The total lumped mass matrix for dynamic vibrations using FEM approach is____________
20. A bar of length L is divided into two elements of equal lengths. If A is the area, E, Youngs
modulus, , the density, the total consistent mass matrix is given by_____________
-oOo-