Maximum shear stress in an assymetric cross-section

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Discussion Overview

The discussion revolves around the calculation of maximum shear stress in asymmetric cross-sections, particularly focusing on L sections. Participants explore the applicability of existing formulas for shear stress in the context of non-symmetric geometries, questioning whether analytical methods can be employed for these cases.

Discussion Character

  • Exploratory
  • Technical explanation
  • Debate/contested

Main Points Raised

  • One participant states the formula for average shear stress and maximum shear stress, noting that the latter is typically limited to symmetric cross-sections.
  • Another participant questions the loading conditions of the L section, suggesting that the orientation of the load could affect the analysis.
  • A participant expresses uncertainty about the ability to calculate maximum shear stress in asymmetric sections, citing a lack of confirmation in various references.
  • One participant encourages exploration of the problem, suggesting that working through it could yield valuable insights.
  • Another participant asserts that it is indeed possible to calculate shear in asymmetric cross-sections, referencing a specific text that addresses the topic in detail.

Areas of Agreement / Disagreement

Participants do not reach a consensus on the methods for calculating maximum shear stress in asymmetric cross-sections, with some expressing uncertainty and others asserting that it is possible based on specific literature.

Contextual Notes

Participants note the limitations of existing literature regarding asymmetric cross-sections and the need for further exploration of loading conditions and analytical methods.

FEAnalyst
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TL;DR
Is it possible to calculate maximum shear stress due to bending of a beam with assymetric cross-section analytically ?
Hi,

the formula for average shear stress in cross-section due to bending is simple: $$\tau=\frac{V}{A}$$
There’s also a formula for maximum shear stress in cross-section: $$\tau_{max}=\frac{VQ}{Ib}$$
But, from what I know, this equation is limited to symmetric cross-sections (rectangular, I section, T section and so on). What about the asymmetric sections such as the L section ? Is it possible to calculate maximum shear stress analytically in such case ?
 
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If we talk about an L section (an angle), how will it be loaded? Parallel to one of the sides (in which case you have non-principal axis bending), or will it be loaded along a principal axis?
 
To be honest, I didn't think about it. I just wonder if it's possible to calculate maximum shear stress in asymmetric cross-sections because all examples I've seen are symmetric in at least one axis. I've checked various books but none of them confirms nor denies that.
 
FEAnalyst said:
To be honest, I didn't think about it. I just wonder if it's possible to calculate maximum shear stress in asymmetric cross-sections because all examples I've seen are symmetric in at least one axis. I've checked various books but none of them confirms nor denies that.
Then this is a prime opportunity to work it out for yourself. No telling what you may learn in the process!
 
Yes, it is possible. My copy of Aircraft Structures by Peery has a chapter titled Beams With Unsymmetrical Cross Sections that discusses how to calculate shear in detail.
 

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