Shear stress in thin wall beams

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SUMMARY

The discussion focuses on calculating shear stress in thin wall beams at specific points A, B, and C using sectioning planes aa, bb, and cc. The formulas provided include Shear Stress(Flange) = q(Flange)/thickness(Flange) and Shear Stress(Web) = q(Web)/thickness(Web), where q is derived from VQ/I. Key insights include that the highest shear stresses occur in the thinnest material and that shear stress is zero at free ends of the section. Understanding which portion of the beam to consider as A' is crucial for accurate calculations.

PREREQUISITES
  • Understanding of shear stress calculations in structural engineering
  • Familiarity with the concepts of sectioning planes in beam analysis
  • Knowledge of the shear force (V) and moment of inertia (I) in beam theory
  • Basic principles of mechanics of materials, particularly regarding thin-walled structures
NEXT STEPS
  • Study the derivation and application of the shear stress formula τ = VQ / (I t)
  • Learn about the significance of the neutral axis in beam analysis
  • Explore advanced topics in thin-walled beam theory and their applications
  • Investigate software tools for beam analysis, such as ANSYS or SolidWorks
USEFUL FOR

This discussion is beneficial for structural engineers, mechanical engineers, and students studying mechanics of materials, particularly those focusing on shear stress analysis in thin-walled beams.

princejan7
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Homework Statement


http://postimg.org/image/9va37id55/
The question is to find the shear stress at the points A, B and C. The solution uses the sectioning planes aa, bb and cc to do so.

For example, at C, how should I know whether to use a horizontal or vertical sectioning plane. Also, how should I know which portion of the beam i would have to consider as A', the bit to the left or right of the sectioning plane ?

Homework Equations



Shear Stress(Flange) = q(Flange)/thickness(Flange)
where q(flange) = VQ(Flange)/I

Shear Stress(Web) = q(Web)/thickness(Web)
where q(Web) = VQ(Web)/I

V is the transverse shear force
Q = A'y" is the first area moments of the area A' with respect to the neutral axis

The Attempt at a Solution

 
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princejan7 said:

Homework Statement


http://postimg.org/image/9va37id55/
The question is to find the shear stress at the points A, B and C. The solution uses the sectioning planes aa, bb and cc to do so.

For example, at C, how should I know whether to use a horizontal or vertical sectioning plane.

Generally, you have the highest shear stresses acting on the thinnest material.

For example, the shear stress τ = VQ / (I t), so for a given shear force V, the smaller t is, the higher the stress τ.

Also, how should I know which portion of the beam i would have to consider as A', the bit to the left or right of the sectioning plane ?
The shear stress will be zero at any free ends of the section. Start from the nearest free end and work toward the section plane at which you wish to calculate the shear stress.
 

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