Ph.D. Preliminary Examination Analysis

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UNIVERSITY OF CALIFORNIA, BERKELEY Spring Semester 2017 Dept. of Civil and Environmental Engineering Structural Engineering, Mechanics and Materials Name:......................................... Ph.D. Preliminary Examination Analysis Note: 1. Dimensions, properties and loading are given in consistent units in all problems. 2. All figures are drawn to scale. 3. Calculations should be shown in detail with all intermediate steps; it is recommended to manipulate expressions symbolically as far as possible and substitute numbers only at or near the end. 1

1. Problem (50% weight) The continuous beam over two spans in Fig. 1 is subjected to a concentrated force P v at the middle of each span. The left span of length 2L has flexural stiffness EI 1 and the second span also of length 2L has flexural stiffness EI 2. P v P v L L L L Figure 1: Continuous beam over two spans The analysis of the continuous beam over two spans under the given load pattern gives a bending moment in the middle of the left span of 0.23992P v L and a bending moment in the middle of the right span of 0.3544P v L. You are asked to answer the following questions: 1. Determine the stiffness ratio EI 1 /EI 2. 2. Determine the vertical deflection under the concentrated force of the left span in terms of P v, L and EI 1. 2

2. Problem (50% weight) The structural model in Fig. 2 consists of five frame elements a through e. The frame elements have very large axial capacity and the following flexural capacity values M p : elements a, b and e have flexural capacity M p of 250 units, element c has flexural capacity M p of 300 units, and element d has flexural capacity M p of 350 units. Fig. 2 shows the location of the plastic hinges at incipient collapse: they form at both ends of element a, end j of element b, both ends of element c, and end j of element e noting that end i corresponds to the lower numbered node to which the element connects. 3 b 50 d 5 e 50 6 2 c 4 6 2 10 a 1 6 6 Figure 2: Simply supported girder with flexibly supported overhang You are asked to answer the following questions: 1. Determine the collapse load factor λ c under the given load pattern. 2. Draw the bending moment diagram of the structure at incipient collapse in Fig. 3 and supply all bending moment values in the figure. 3. Determine the vertical support reaction at node 6. 3

6 2 10 6 6 Figure 3: Bending moment diagram 6 2 10 6 6 Figure 4: Auxiliary figure 4

6 2 10 6 6 Figure 5: Auxiliary figure 5

UNIVERSITY OF CALIFORNIA, BERKELEY Fall Semester 2016 Dept. of Civil and Environmental Engineering Structural Engineering, Mechanics and Materials Name:......................................... Ph.D. Preliminary Examination Analysis Note: 1. Dimensions, properties and loading are given in consistent units in all problems. 2. All figures are drawn to scale. 3. Calculations should be shown in detail with all intermediate steps; it is recommended to manipulate expressions symbolically as far as possible and substitute numbers only at or near the end. 4. Results involving multiplication or division with a matrix larger than 2 x 2 will not receive credit. 1

1. Problem (50% weight) The structural model in Fig. 1 of a braced frame consists of three inextensible frame elements a, b, and c and a truss (brace) element d. The flexural section stiffness EI of the frame elements a, b and c is 100,000, while the axial section stiffness EA of the brace element d is 40,000 units. The structure is subjected to a downward vertical nodal force of 50 units at node 2, as Fig. 1. In addition, the brace element d is prestressed with an initial prestressing force q 0 = 100. 1 a 2 50 d b 3 6 6 c 4 Figure 1: Braced frame geometry and loading You are asked to answer the following questions: 1. Draw the bending moment distribution in Fig. 2. 2. Determine the node translations and draw the deformed shape in Fig. 3. Figure 2: Bending moment distribution Figure 3: Deformed shape 2

2. Problem (50% weight) The continuous girder in Fig. 4 over two equal spans of length 2L is subjected to a uniform element load w that extends over the left half of each span, as Fig. 4 shows. The continuous girder has uniform flexural stiffness EI. w w L L L L Figure 4: Two span continuous girder geometry and loading You are asked to answer the following questions: 1. Propose a suitable discrete structural model for determining the bending moment distribution of the continuous girder under consideration of the rule that division and multiplication with matrices larger than 2x2 is not allowed for hand calculations. 2. Determine and draw the bending moment distribution under the given loading in Fig. 5. 3. Determine the vertical translation at the middle of the right span of the continuous girder. L L L L Figure 5: Bending moment distribution 5