Please answer this question. Make sure to explain your answer step-by-step so that I can understand it clearly, and Please note that this is not a marked question, The rigid bar ABCD is consist of two cylindrical portions AC and CD shown in FigureQ1.1. Cylindrical rod AC is made of aluminum (E-70 GPa) and has a cross-sectionalarea of 581 mm² whereas cylindrical rod CD is made of steel (E = 200 GPa) and has across-sectional area of 194 mm². It is noted that loads are applied at three distinctpositions at point B, C and D along the length of the rod.(a)A = 581 mm²B300 kN(b)300 mmA = 194 mm²300 mmс/180 kN400 mmD120 kNFigure Q1.1Prepare finite element model consisting of 3 elements for the bar ABCD. Clearlydefine all the nodes, elements, constraint and loads of the model.(b) Using elemental description, determine the global stiffness matrix and loadmatrix to present the entire problem. Write them in general form following thefinite element formulation, [K]{U} = {F}.(a) Calculate the displacements at points B, C and D.38Determine the total deformation of the rigid bar ABCD under the applied loads.

Consider the bar ABCD is discritised into three elements and represent the forces acting as…

The rigid bar ABCD is consist of two cylindrical portions AC and CD shown in Figure Q1.1. Cylindrical rod AC is made of aluminum (E-70 GPa) and has a cross-sectional area of 581 mm² whereas cylindrical rod CD is made of steel (E-200 GPa) and has a cross-sectional area of 194 mm². It is noted that loads are applied at three distinct positions at point B, C and D along the length of the rod. (a) (b) A=581 mm² B (b) A = 194 mm² 300 kN 300 mm 300 mm C 180 KN 400 mm D 120 kN Figure Q1.1 Prepare finite element model consisting of 3 elements for the bar ABCD. Clearly define all the nodes, elements, constraint and loads of the model. Using elemental description, determine the global stiffness matrix and load matrix to present the entire problem. Write them in general form following the finite element formulation, [K] {U} = {F}. (a) Calculate the displacements at points B, C and D. Determine the total deformation of the rigid bar ABCD under the applied loads.

The rigid bar ABCD is consist of two cylindrical portions AC and CD shown in Figure Q1.1. Cylindrical rod AC is made of aluminum (E-70 GPa) and has a cross-sectional area of 581 mm² whereas cylindrical rod CD is made of steel (E-200 GPa) and has a cross-sectional area of 194 mm². It is noted that loads are applied at three distinct positions at point B, C and D along the length of the rod. (a) (b) A=581 mm² B (b) A = 194 mm² 300 kN 300 mm 300 mm C 180 KN 400 mm D 120 kN Figure Q1.1 Prepare finite element model consisting of 3 elements for the bar ABCD. Clearly define all the nodes, elements, constraint and loads of the model. Using elemental description, determine the global stiffness matrix and load matrix to present the entire problem. Write them in general form following the finite element formulation, [K] {U} = {F}. (a) Calculate the displacements at points B, C and D. Determine the total deformation of the rigid bar ABCD under the applied loads.

Mechanics of Materials (MindTap Course List)

9th Edition

ISBN:9781337093347

Author:Barry J. Goodno, James M. Gere

Publisher:Barry J. Goodno, James M. Gere

Chapter2: Axially Loaded Members

Section: Chapter Questions

Problem 2.4.17P: A bimetallic bar (or composite bar) of square cross sec lion with dimensions 2b X lb is construe ted...

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