What condition defines a principal stress?

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SUMMARY

Principal stresses are defined as normal stresses that occur in a given stress state, specifically in materials under tension or bending. In the case of a thin plate subjected to tensile stress, the principal stresses act normal to the sides of the plate. For a beam with a rectangular cross-section in pure bending, the principal stresses correspond to the bending stresses, manifesting as tensile and compressive stresses on the beam's surfaces. Mohr's Circle is utilized for calculating principal and shear stresses in more complex geometries, such as I-beams.

PREREQUISITES
  • Understanding of solid mechanics principles
  • Familiarity with stress and strain concepts
  • Knowledge of Mohr's Circle for stress analysis
  • Basic engineering mechanics, particularly bending and tensile stress
NEXT STEPS
  • Study the application of Mohr's Circle in stress analysis
  • Learn about the derivation of principal stresses in various geometries
  • Explore the effects of different loading conditions on principal stresses
  • Investigate the relationship between shear and principal stresses in materials
USEFUL FOR

Engineering students, structural engineers, and professionals involved in material stress analysis will benefit from this discussion, particularly those focusing on solid mechanics and structural integrity.

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What condition defines a principal stress?

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Since I'm studying Engineering I should probably be able to explain this to you in my own words, but this site does a good job of it:
http://www.efunda.com/formulae/solid_mechanics/mat_mechanics/plane_stress_principal.cfm

If you consider a given stress state, principal stresses are defined as stresses that are normal stresses only. So take the easy case of a thin plate, and apply a tensile stress to one end (i.e. try to stretch it). In that case, the principal stresses would be normal to the sides of the plate. If you had a beam with a rectangular cross section in pure bending, the principal stresses would just be equal to the bending stresses, and are tensile and compressive stresses on the top and bottom surface of the beam, assuming you've got a point force (for example) P acting normal to the bottom surface (in the positive direction, bending the beam into an upside down U). Things like I beams are a little different, and in that case you use Mohr's Circle to calculat principal stresses and shear stresses; the website covers that in a good amount of detail.

If I've missed anything or explained anything ambiguously, someone let me know and I'll try to do a better job of it. :P
 
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this covers the confution I had, thank you verry much

Loki1342 said:
Since I'm studying Engineering I should probably be able to explain this to you in my own words, but this site does a good job of it:
http://www.efunda.com/formulae/solid_mechanics/mat_mechanics/plane_stress_principal.cfm

If you consider a given stress state, principal stresses are defined as stresses that are normal stresses only. So take the easy case of a thin plate, and apply a tensile stress to one end (i.e. try to stretch it). In that case, the principal stresses would be normal to the sides of the plate. If you had a beam with a rectangular cross section in pure bending, the principal stresses would just be equal to the bending stresses, and are tensile and compressive stresses on the top and bottom surface of the beam, assuming you've got a point force (for example) P acting normal to the bottom surface (in the positive direction, bending the beam into an upside down U). Things like I beams are a little different, and in that case you use Mohr's Circle to calculat principal stresses and shear stresses; the website covers that in a good amount of detail.

If I've missed anything or explained anything ambiguously, someone let me know and I'll try to do a better job of it. :P
 
Last edited by a moderator:

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