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Step 6: Results
Total Deformation
First, examine the total deformation by clicking on the Total Deformation button, . If you have used only two elements, you should see the output shown below.
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https://confluence.cornell.edu/download/attachments/125812731/2elemtotaldef_full.png
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https://confluence.cornell.edu/download/attachments/125812731/10elemtotdef_full.png
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Plot Deformed Shape of Midline
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<iframe width="560" height="315" src="https://www.youtube.com/embed/Zf9zYFNXkaI" frameborder="0" allowfullscreen></iframe> |
Plot Bending Stress
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<iframe width="560" height="315" src="https://www.youtube.com/embed/_04tFkcaqXw" frameborder="0" allowfullscreen></iframe> |
Plot Bending Moment
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<iframe width="560" height="315" src="https://www.youtube.com/embed/t2uTPPyIVEI" frameborder="0" allowfullscreen></iframe> |
Probe Displacement
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<iframe width="560" height="315" src="https://www.youtube.com/embed/SA-rmkqkbm0" frameborder="0" allowfullscreen></iframe> |
Check Your Understanding
Select the correct option below.
Consider the case where we replace our square cross-section in ANSYS with an I-shaped cross-section that is taller, has a lower cross-sectional area and the same moment of inertia. If we then re-solve the problem in ANSYS, which of the following results would be affected? Select all options that apply.
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Maximum Bending Stress
For this static structural problem, the maximum bending stress is of interest. In order to examine the maximum bending stress first expand the Beam Tool folder, , which is located under "Solution(A6)". Next, click on the Maximum Bending Stress button, . If you have used only two elements, you should obtain the following output.
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https://confluence.cornell.edu/download/attachments/125812731/2elemmaxbend_full.png
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Deformed shape of the midline, u_y(x)
Max. bending stress at root
Go to Step 7: Verification & ValidationSee and rate the complete Learning Module