x7=12KN , x8=19kN/m, x4=4m, x5=39m, x6=5m,
x7=12KN , x8=19kN/m, x4=4m, x5=39m, x6=5m, Q2. In the 3-span beam shown in the Figure 2, the...
Analyse the 3 span beam shown in the Figure below by the method of moment distribution and draw the bending moment and shear force diagrams. You need not show the maximum values of the bending moments in the spans. El can be assumed to be a constant across all the members. 24 kN/m 36 kN/m X2 kN/m 8m X3 m XIm X1 X2 X3 6m 38 kN/m 8m
A continuous beam ABC shown in Figure 2 is fixed at A. Supports at B and C are rollers. A uniform distributed load 40kN/m is applied force acts downward on the span of BC as shown in Figure 2. The EI of the beam is over the span of AB and a 60kN constant (a) Determine the internal moments at A and B using the slope-deflection method [10 marks] (b) Draw the bending values of bending (c) Sketch the deformed...
The beam is shown in the figure below. Use the slope-deflection method. The support Ais pinned, support B is a roller, and support C is fixed. Assume El = 21537 kNm2. The support at B settles by 73 mm (downwards). The segment AB is subjected to a uniformly distributed load w= 11 kN/m. The segment BC is subjected to a point load P = 91 KN. Enter the digit one in the answer box. The link will be provided on...
Consider the beam shown in the figure: (12 marks] a- Use the section method to draw the shear force and bending moment diagrams for the beam shown. Label all significant points on each diagram. And identify the maximum moments along with their respective locations. [10 marks] b- Determine V and M in the beam at a point located 1.50 m to the right of B. [1 mark] C- Determine V and M in the beam at a point located 1.25...
3 (a) For the beam shown in Figure Q3.1, E 200GPa and I 22:10 m throughout. By using the stiffness method and neglecting axial effects: (i) Calculate the rotations of each of the supports [5 marks (ii) Calculate the bending moment and shear force diagrams. [10 marks] (iii) Calculate the reactions and check equilibrium. [5 marks] 7.5kNm SkNm 2 2 Im Im Figure Q3.1 3 (a) For the beam shown in Figure Q3.1, E 200GPa and I 22:10 m throughout....
3 (a) For the beam shown in Figure Q3.1, E 200GPa and I 22:10 m throughout. By using the stiffness method and neglecting axial effects: (i) Calculate the rotations of each of the supports [5 marks (ii) Calculate the bending moment and shear force diagrams. [10 marks] (iii) Calculate the reactions and check equilibrium. [5 marks] 7.5kNm SkNm 2 2 Im Im Figure Q3.1 3 (a) For the beam shown in Figure Q3.1, E 200GPa and I 22:10 m throughout....
Need help with E and F please. 3. The beam shown in the figure below is carrying superimposed dead load of 25 kN/m and use and occupancy load of 45 kN/m. For preliminary analysis, assume a self weight of 10 kN/m. We are required to find the maximum positive (tension at the bottom) and negative (tension at the top) moments due to the factored loads, and then design the beam CIV E 374-RC-Lab 3 Fall 2018 (a) Determine the maximum...
Question 1 (Total 100/3 Marks) Figure 1 (all units are mm) shows a simply supported beam of span 2500 mm with a 5 kN/m load. The cross-section of the beam is a composite section made from two steel plates attached to the top and bottom of a timber section. The top steel plate is 5 mm wide and 20 mm deep. The bottom steel plate is also 5 mm wide but 10 mm deep. The timber section is 50 mm...
Problem 3: One way solid slab (10 pts) The slab shown in Figure 2 is 200 mm thick. All beams/girders have 400 x 600 mm sections. All columns have 400 x 400 mm sections. Superimposed dead load = 3 kN/m, live load = 4 kN/mº. No walls used. a) Check the slab thickness for deflection control. b) Determine the ultimate uniform load on a l-m wide typical slab strip. c) Determine the ultimate uniform load transferred to beam 2. d)...