Subject Code: 2160609
GUJARAT TECHNOLOGICAL UNIVERSITY
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BE- SEMESTER-VI (NEW) EXAMINATION - WINTER 2020Subject Name: Computational Mechanics
Time: 02:00 PM TO 04:00 PM
Instructions:
- Attempt any THREE questions from Q.1 to Q.6.
- Q.7 is compulsory.
- Make suitable assumptions wherever necessary.
- Figures to the right indicate full marks.
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Q.1
- (a) Derive member stiffness matrix of beam member. (03)
- (b) Derive the relationship As = RTAw for rotation of axis in 2D. (04)
- (c) Using member stiffness approach, determine joint displacement for the beam loaded as shown in fig.1. Take EI = 60 kNm². (07)
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Q.2
- (a) Explain symmetry and anti-symmetry with neat sketches. (03)
- (b) Write rotation matrices of plane truss member and plane frame member. (04)
- (c) Using member stiffness approach, determine joint displacements for the beam loaded as shown in fig.1, if the support ‘A’ rotates by 10° counter-clockwise. Take EI = 60 kNm². (07)
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Q.3
- (a) Evaluate member stiffness matrices of the truss shown in fig.3. (03)
- (b) Evaluate joint displacements of the truss shown in fig.3. (04)
- (c) Determine member forces of the truss shown in fig.3. (07)
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Q.4
- (a) Define stiffness and flexibility. (03)
- (b) Determine member stiffness matrices of the plane frame shown in fig.4. Take EI = 60 kNm², EA = 3435 kN. (04)
- (c) Determine joint displacements and support reactions of the plane frame shown in fig.4. Take EI = 60 kNm², EA = 3435 kN. (07)
Q.5
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- (a) Write steps of finite element analysis. (03)
- (b) Derive shape functions of CST element using Cartesian coordinate. (04)
- (c) Using FEM, evaluate nodal displacements of the bar shown in fig.5. Take E = 2 x 105 N/mm². (07)
Q.6
- (a) Write displacement functions for 1D and 2D elements. (03)
- (b) Using FEM, evaluate nodal displacements of the beam shown in fig.6. Take EI = 60 kNm². (04)
- (c) Using FEM, evaluate nodal displacements and element stresses for the bar shown in fig.7. Take EA = 500 kN. (07)
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Q.7
- (a) Define plane stress and plane strain problems. Write constitutive matrices of plane stress and plane strain problems. (05)
- (b) OR Derive nodal load vector for the 2-noded bar element subjected to surface traction ‘T’ per unit length. (05)
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Date: 03/02/2021
Total Marks: 47
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