Maximum shear stress in an assymetric cross-section

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SUMMARY

The discussion centers on calculating maximum shear stress in asymmetric cross-sections, particularly L sections. The standard formula for maximum shear stress, $$\tau_{max}=\frac{VQ}{Ib}$$, is typically applicable to symmetric cross-sections. However, it is confirmed that it is possible to analytically calculate maximum shear stress in asymmetric sections, as detailed in the book "Aircraft Structures" by Peery, which includes a chapter specifically addressing beams with unsymmetrical cross-sections.

PREREQUISITES
  • Understanding of shear stress formulas, specifically $$\tau=\frac{V}{A}$$ and $$\tau_{max}=\frac{VQ}{Ib}$$
  • Familiarity with cross-sectional geometry, particularly asymmetric shapes like L sections
  • Knowledge of bending principles and loading conditions in structural engineering
  • Access to "Aircraft Structures" by Peery for in-depth study
NEXT STEPS
  • Study the chapter on Beams With Unsymmetrical Cross Sections in "Aircraft Structures" by Peery
  • Research methods for calculating shear stress in asymmetric cross-sections
  • Explore software tools for structural analysis that handle asymmetric sections
  • Learn about principal axis bending and its implications for shear stress calculations
USEFUL FOR

Structural engineers, civil engineers, and students studying mechanics of materials who are interested in advanced shear stress calculations in asymmetric cross-sections.

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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