For the configuration shown in Figure P6.11, determine the deflection at the point of load application using a one-element model. If a mesh of several triangular elements is used, comment on the stress values in the elements close to the tip.
For the configuration shown in Figure P6.11, determine the deflection at the point of load application using a one-element model. If a mesh of several triangular elements is used, comment on the stress values in the elements close to the tip.
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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Transcribed Image Text:6.11 For the configuration shown in Figure P6.11, determine the deflection at the point
of load application using a one-element model. If a mesh of several triangular
elements is used, comment on the stress values in the elements close to the tip.
2 (0,25
25 mm
(0,0)
35 mm
90 N
Figure P6.11
1 (35,25)
t = 8 mm
E = 69,900 MPa
v = 0.3
45 N
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Step 1: Write the given data and what is to find
VIEWStep 2: Assign the nodes and prepare the parameter table:
VIEWStep 3: Write the element stiffness matrix for both the elements:
VIEWStep 4: Write the global stiffness matrix:
VIEWStep 5: Write the boundary conditions and determine the nodal displacements at node 2:
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