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A) Given Autodesk inventor and Ansys software, write one paragraph summary each to describe how you would conduct a simple simulation. B) A truss assemblage shown in Figure 3, in which node A experiences a downward load of 18 kN, lies in the global x-y coordinate. If, A = 2.5x10* m², E = 200 GPa for all elements, use the direct stiffness method to: i) Assemble the global stiffness matrix. ii) Solve for the nodal displacements. ii) Compute the stresses in the elements.

A) Given Autodesk inventor and Ansys software, write one paragraph summary each to describe how you would conduct a simple simulation. B) A truss assemblage shown in Figure 3, in which node A experiences a downward load of 18 kN, lies in the global x-y coordinate. If, A = 2.5x10* m², E = 200 GPa for all elements, use the direct stiffness method to: i) Assemble the global stiffness matrix. ii) Solve for the nodal displacements. ii) Compute the stresses in the elements.

Elements Of Electromagnetics
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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-450 - 450 –→-350 y"D B 600 18 KN Figure 3 A) Given Autodesk inventor and Ansys software, write one paragraph summary each to describe how you would conduct a simple simulation. B) A truss assemblage shown in Figure 3, in which node A experiences a downward load of 18 kN, lies in the global x-y coordinate. If, A = 2.5x10* m², E = 200 GPa for all elements, use the direct stiffness method to: i) Assemble the global stiffness matrix. ii) Solve for the nodal displacements. ii) Compute the stresses in the elements. 2.
Transcribed Image Text:-450 - 450 –→-350 y"D B 600 18 KN Figure 3 A) Given Autodesk inventor and Ansys software, write one paragraph summary each to describe how you would conduct a simple simulation. B) A truss assemblage shown in Figure 3, in which node A experiences a downward load of 18 kN, lies in the global x-y coordinate. If, A = 2.5x10* m², E = 200 GPa for all elements, use the direct stiffness method to: i) Assemble the global stiffness matrix. ii) Solve for the nodal displacements. ii) Compute the stresses in the elements. 2.
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