; For the frame shown below, determine the degree of indeterminacy and compute the reactions at D. Construct the shear-force and bending moment diagrams and sketch the elastic curve for the beam loaded as shown below. Also determine the shear force and bending moment at point X, 4 m from A. El=constant. 33 KN/m 36 KN/m 24 KN/m |20 KN BT 5 m 6 m 2 m 40 KN IA 6 m 2 m 4 m '2 m A ) Assuming that beams are framed into girders in simple supports as well as the girders are framed into columns with pin connections, determine the maximum moment and the maximum deflection in an interior girder. Consider load pattern. F.. 5) For the truss shown below, determine the bar force of AB and AD. Also indicate if these forces are tension or compression. The live load is 2.40 KPa 30 KN B 3 m C 3 m 6 m 6 m and the dead load consists 13 m only of the weight of beams and girders that No joint 3m 3 m are 1 KN/m and 1.4 KN/m, 3 m respectively. The girders I3 m are made of wide flanges 2 m with depth 400 mm and 3 m I=600x106 mm4. E=200 T3 m 50 KN

; For the frame shown below, determine the degree of indeterminacy and compute the reactions at D. Construct the shear-force and bending moment diagrams and sketch the elastic curve for the beam loaded as shown below. Also determine the shear force and bending moment at point X, 4 m from A. El=constant. 33 KN/m 36 KN/m 24 KN/m |20 KN BT 5 m 6 m 2 m 40 KN IA 6 m 2 m 4 m '2 m A ) Assuming that beams are framed into girders in simple supports as well as the girders are framed into columns with pin connections, determine the maximum moment and the maximum deflection in an interior girder. Consider load pattern. F.. 5) For the truss shown below, determine the bar force of AB and AD. Also indicate if these forces are tension or compression. The live load is 2.40 KPa 30 KN B 3 m C 3 m 6 m 6 m and the dead load consists 13 m only of the weight of beams and girders that No joint 3m 3 m are 1 KN/m and 1.4 KN/m, 3 m respectively. The girders I3 m are made of wide flanges 2 m with depth 400 mm and 3 m I=600x106 mm4. E=200 T3 m 50 KN

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

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