GTU Civil Engineering (Semester 5)
Structural Analysis - 3
December 2014
Total marks: --
Total time: --
INSTRUCTIONS
(1) Assume appropriate data and state your reasons
(2) Marks are given to the right of every question
(3) Draw neat diagrams wherever necessary


1 (a) Explain term 'Plastic hinge'. State (i) Upper bound theorem and (ii) Lower bound theorems for collapse load in plastic analysis.
7 M
1 (b) Discuss the characteristics of stiffness matrix. Formulate Stiffness matrix [S] for a prismatic cantilever beam, of length 'L', also considering axial deformation with usual notations. Take EI = Constant.
7 M

2 (a) Derive formula for meridional and hoop force in conical dome subjected to concentrated load 'W' at the vertex, with usual notations.
7 M
2 (b) Derive formulae of shear force, bending moment and torsional moment at any section, for the quarter circular cantilever beam curved in plan, subjected to uniformly distributed load w per unit run throughout its length, with usual notations.
7 M
2 (c) Find Shape factor for the section shown in fig. (i)

7 M

3 (a) Formulate the flexibility matrix [F] and vector {DQL} for the beam shown in fig. (ii). Assume fixed end moment at A and internal moment at support B as redundant Q1 and Q2 respectively.

7 M
3 (b) For the beam (given in Q.3(a) above), calculate values of all unknown reactions using flexibility method. Also draw SF and BM diagram.

7 M
3 (c) A circular beam curved in plan is symmetrically supported on six columns. The radius of beam is 6 m and is subjected to UDL of 5 kN/m throughout its length. Determine the value of shear force, bending moment and torsional moment at φ =0°, φ = 30° and φ =60°. (Mid span and Supports)
7 M
3 (d) Determine collapse load in terms of Mp for the portal frame loaded as shown in fig. (iii)

7 M

4 (a) Formulate the stiffness matrix [S] and load vector {AD ? ADL}for the beam shown in fig. (ii).

7 M
4 (b) For the beam (given in Q.4(a) above), calculate joint displacement and final end moments using stiffness method.

7 M
4 (c) A conical dome of 6 m diameter and central rise of 4 m supports total UDL including self weight of 10 kN/m2 over the entire surface. The thickness of dome is 100 mm. Calculate meridional stress and hoop stress at the base of the dome.
7 M
4 (d) Define term 'collapse load'. Determine collapse load in terms of Mp, using static method for the beam fixed at both ends and subjected to UDL 'w' kN/m throughout its length 'L' m as shown in fig. (iv).

7 M

5 (a) A spherical dome having 8 m span and 2 m rise, subjected to UDL of 10 kN/m2 including self weight. The thickness of the dome is 100 mm. Calculate meridional and hoop stresses at each θ = 10° interval from crown to base of the dome.
7 M
5 (b) A beam curved in plan is fixed at both the ends. The radius of the beam is 5 m and subtended angle is 75°. It is subjected to UDL of 10 kN/m throughout its length. If the section of the beam is 230 mm × 600 mm, determine shear force, bending moment and torsional moment at mid span and end supports. Take EI = 5.608GJt.
7 M
5 (c) Discuss various types of stresses in spherical domes with sketch. Using formula of hoop force prove that in a spherical dome, subjected to UDL over entire surface, the hoop force changes its nature at an angle 51.83° from crown.
7 M
5 (d) A semi-circular beam curved in plan is supported on three equally spaced supports, carries UDL of w per unit run throughout its length. The radius of the beam is 'r'. Determine maximum value of bending and torsional moment.
7 M



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