Stress components on cantilever beam loaded off symmetry

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SUMMARY

The discussion focuses on calculating the stress components of a cantilever beam loaded off symmetry, specifically at the point x=0, y=h/2, z=0. The primary equation used is σ=My/I, where M represents the moment and I is the moment of inertia. Participants emphasize the importance of breaking down the transverse load into its components to accurately determine bending stress. It is concluded that shear stress may arise from the load components, and the analysis should consider each load individually to clarify the effects on the beam.

PREREQUISITES
  • Understanding of cantilever beam mechanics
  • Familiarity with shear and bending moment diagrams
  • Knowledge of stress analysis equations, specifically σ=My/I
  • Experience with resolving forces into components
NEXT STEPS
  • Study the calculation of moment of inertia (Ixx and Iyy) for various beam shapes
  • Learn how to construct shear and bending moment diagrams for cantilever beams
  • Explore the effects of transverse loads on beam stress analysis
  • Investigate the principles of pure bending and its assumptions in beam theory
USEFUL FOR

Engineering students, structural analysts, and professionals involved in mechanical design and stress analysis of beams will benefit from this discussion.

habibi69
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Homework Statement


An element is taken from the wall end of the cantilever beam that is loaded as per the diagram. What are the stress components of the element, taken at x=0, y=h/2, z=0

oW1iF65.jpg

Homework Equations


σ=My/I

The Attempt at a Solution


So from the shear moment diagram, the moment and shear at the wall end are found but then I'm not too sure what to do about the transverse load at an angle. I broke the load down into it's components but I'm not sure what to do about it.
 
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You will just need to find the bending stress using each of the components of P. So you will need to get Ixx and Iyy for the beam and find Mxx and Myy for each of the components of P.

So

σx= (Mxxy)/Ixx


(xx denotes about the x-axis and yy about the y-axis)
 
So is there no stress on the z face, σ_{z} ?
 
habibi69 said:
So is there no stress on the z face, σ_{z} ?

Think about what happens when you resolve P into its components.
 
So then there would also be a shear stress caused by the load right? I'm getting confused now

Unless we assume that the beam is under pure bending, then there would be no shear
 
Last edited:
It might be better if you look at the beam loaded by each of the components of P individually. Draw the shear and bending moment diagrams without worrying too much about how everything acts simultaneously.
 

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