QUESTION ONE (STATICALLY DETERMINATE BEAMS)Use Figure 1 to answer the following questions. (Show all your calculations)Calculate:a) Reactions (Ax, Ay and Cy)b) Shear function, x-intercepts and moment functions between A and Bc) Shear function, x-intercepts and moment function between B and Cd) Draw the shear and bending moment diagrams for the beam shown below.Highlight/Underline your answers.30 kN/mA-6.5 m20 kN-FIGURE 1: UNEQUAL TRIANGULAR DISTRIBUTED LOADED BEAM12 kNQUESTION TWO (STATICALLY DETERMINATE TRUSSES)Determine the force in each member of the truss shown by the method of joints.Redraw the Truss given in Figure 2 and write all your answers on the Truss as in Figure4.19 (b) in Kassimalli textbook.B12 kN12 kNIL M40 kN40 kN-5 at 3 m 15 m40 kN-GECA12 kNNHFDB10 m→Figure 2: Truss12 kN 12 kNP4 m4m45 kN/mC4 m4 m

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QUESTION ONE (STATICALLY DETERMINATE BEAMS) Use Figure 1 to answer the following questions. (Show all your calculations) Calculate: a) Reactions (Ax, Ay and Cy) b) Shear function, x-intercepts and moment functions between A and B c) Shear function, x-intercepts and moment function between B and C d) Draw the shear and bending moment diagrams for the beam shown below. Highlight/Underline your answers. 30 kN/m A -6.5 m B TITT]: 10 m- 45 kN/m C FIGURE 1: UNEQUAL TRIANGULAR DISTRIBUTED LOADED BEAM

QUESTION ONE (STATICALLY DETERMINATE BEAMS) Use Figure 1 to answer the following questions. (Show all your calculations) Calculate: a) Reactions (Ax, Ay and Cy) b) Shear function, x-intercepts and moment functions between A and B c) Shear function, x-intercepts and moment function between B and C d) Draw the shear and bending moment diagrams for the beam shown below. Highlight/Underline your answers. 30 kN/m A -6.5 m B TITT]: 10 m- 45 kN/m C FIGURE 1: UNEQUAL TRIANGULAR DISTRIBUTED LOADED BEAM

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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Design of structures using FEA

An arrangement, in which various members are interconnected with their constrained relative motion, the whole arrangement is then known as a structure. The degree of freedom of such a structure is zero. In such a structure, the load can act throughout the length of the structure or at the joints.

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