How Do You Calculate Displacement for an Irregular Cantilever Beam?

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SUMMARY

This discussion focuses on calculating the displacement of an irregular cantilever beam with three segments, each having different moment inertias: I_1 for the horizontal segment, I_2 for the diagonal segment, and I_3 for the end diagonal segment. The calculation involves using the equation M_x = EI * d^2y/dx^2 and integrating to find displacement. The procedure includes calculating flexure and deflection for each segment, determining curvature, and summing deflections to find the total displacement at point D. The geometry of the beam significantly influences the calculations, particularly the moment inertia values.

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timmy996
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Hello,

I am trying to figure out how to calculate displacement for an irregular cantilever beam, i.e. one that is not the normal straight-beam that you would see in a textbook.

Please see the attached image. If the left end is fixed, and I want to calculate the displacement of point A due to an applied force at that point, how would I go about it?

Are you still able to use M_x = EI * d^2y/dx^2 and solve for displacement by integrating? I am not exactly sure how the geometry of the weird bended shape comes into play. Thanks.

- T
 

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The cantilever beam has three segments:
1) Horizontal segment with moment inertia I_1
2) Diagonal segment at middle with moment inertia I_2
3) Diagonal segment at end with moment inertia I_3

Note: I_2 is determined relative to global Y axis (not local Y axis). Thus, I_2>I_1 as illustrated. I_3 is not required for calculations; only its horizontal length is needed.

The beam has four points
A) At support
B) Right of segment 1
C) Right of segment 2
D) Right of segment 3

Procedure:
a) Calculate flexure and deflection over segment 2
b) Calculate flexure and deflection over segment 1
c) Add deflection 1 and 2 to give total deflection at point C
d) Determine curvature at point C
e) Determine tangent of segment 3, and thus deflection of segment 4
f) Add deflection of point step (c) to setup (e) to yield total deflection at (4)
 

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