Normal Stress Vectors: Sketch 1 vs Sketch 2

Click For Summary
SUMMARY

The discussion centers on the behavior of normal stress vectors in relation to material deformation, specifically addressing whether these vectors should remain normal to the surface or align parallel to another surface during deformation. Participants clarify the distinction between the second-order stress tensor and the first-order stress vector, emphasizing the importance of the Cauchy stress relationship in three-dimensional stress analysis. The conversation highlights the invariance of the stress tensor and traction vector across coordinate systems and introduces dyadic tensor notation as a valuable tool for understanding these concepts. Additionally, the implications of small versus large deformations on stress behavior are discussed, particularly in the context of linear material behavior.

PREREQUISITES
  • Cauchy stress tensor
  • Dyadic tensor notation
  • Stress transformation techniques
  • Understanding of linear and non-linear material behavior
NEXT STEPS
  • Study the Cauchy-Green deformation tensor for large deformation analysis
  • Explore dyadic tensor notation in detail for stress analysis
  • Learn about stress transformation methods in three-dimensional contexts
  • Investigate the mathematical principles of linear versus non-linear material behavior
USEFUL FOR

Mechanical engineers, materials scientists, and students studying solid mechanics or continuum mechanics who are interested in the behavior of stress vectors during material deformation.

person123
Messages
326
Reaction score
52
TL;DR
I'm wondering the direction the normal stress should be shown on a deformed material element.
Let's say you have a material element with normal and shear stress. These stresses were computed using stress transformation. When the material deforms, should the normal stress vectors remain normal to the surface (sketch 1) or parallel to the other surface (sketch 2)? Which would be more accurate? Thanks!

20200807_181834.jpg
 
Physics news on Phys.org
A normal stress, by definition, is the component of the stress vector that is normal to the surface. A shear stress is, by definition, a component of the stress vector that is tangent to the surface.

I think you may be confusing the components of the 2nd order stress tensor with the components of the stress vector (first order tensor) on a surface of arbitrary orientation.
 
  • Like
Likes   Reactions: etotheipi
Maybe this would be the question asked more precisely:
Let's say you take the traction vector on that plane. In which case would the sum of the vectors be equal to the traction vector?
 
person123 said:
Maybe this would be the question asked more precisely:
Let's say you take the traction vector on that plane. In which case would the sum of the vectors be equal to the traction vector?
Yes.
 
Does anyone have ideas on this more precise version of the question?
 
person123 said:
Does anyone have ideas on this more precise version of the question?
Are you familiar with the Cauchy stress relationship?
 
Yes. For 3 dimensions, take a matrix whose elements are the stresses on a differential cube in xyz orientation ( rows and columns indicating the plane and direction of stress). That's the cauchy stress tensor. When multiplied by a vector normal to a surface, the output is the traction vector for that surface. That can be decomposed into normal and shear stresses. I'm still unsure how this would work for an already deformed material because there would be another transform for deforming the material.
 
person123 said:
Yes. For 3 dimensions, take a matrix whose elements are the stresses on a differential cube in xyz orientation ( rows and columns indicating the plane and direction of stress). That's the cauchy stress tensor. When multiplied by a vector normal to a surface, the output is the traction vector for that surface. That can be decomposed into normal and shear stresses. I'm still unsure how this would work for an already deformed material because there would be another transform for deforming the material.
That would only be for the components in a change of coordinate system. The stress tensor, the normal to a surface, and the corresponding traction vector are invariant entities, independent of any specific coordinate system and of the components resolved on that coordinate system. Thinking of them in terms of a matrix with rows and columns automatically implies a specific coordinate system.

Do yourself a favor and learn about dyadic tensor notation, which treat tensors as such invariant entities. For a good development of this, see Appendix B of Transport Phenomena by Bird et al. Or see the brief tutorial I presented in post #12 of the following thread: https://www.physicsforums.com/threads/so-tension-is-not-a-force.960204/#post-6089855

You seem to be focusing on using an embedded material coordinate system in describing the deformed material. Is this the case?
 
It just dawned on me...Is it possible that you are talking about situations involving small displacements and small strains, like deformation of solids?
 
  • #10
My apology for the late response.
Chestermiller said:
It just dawned on me...Is it possible that you are talking about situations involving small displacements and small strains, like deformation of solids?
Yes. I'm thinking of solids specifically. I'm also thinking of small displacements in order to ensure stress and strain relations are linear.

Chestermiller said:
That would only be for the components in a change of coordinate system. The stress tensor, the normal to a surface, and the corresponding traction vector are invariant entities, independent of any specific coordinate system and of the components resolved on that coordinate system. Thinking of them in terms of a matrix with rows and columns automatically implies a specific coordinate system.
Yes, although I did have a sense that the stress tensor is independent of coordinate system, I realized that using a matrix does imply a specific coordinate system.

Using dyadics, the stress tensor is a sum of dyadics. Instead of doing matrix multiplication, the tensor is dotted with the normal vector, producing the traction vector. Using the equation you had in your post: $$(\bf v_1 v_2)\cdot v3=v_1(v_2\cdot v_3)$$ In order to ensure that this product is nonzero, ##v_2## must not be orthogonal to ##v_3##, or for unit basis vectors they must be equivalent.

For the question I have though, I'm thinking specifically about change of coordinate systems though.

I thought about my question a bit more. I want to use a bit more of a specific, concrete example. Let's say there's a rod under pure tension in the x direction and you apply a 45 degree cut. There would be a normal and shear stress both half of the normal stress in the x direction. If the material deforms under tension however, the angle changes (let's say to a 30 degree angle). In order to maintain force balance, this would be equivalent to a 30 degree cut:
20200819_195811.jpg

This seems to mean that if you take a section of a material under some stress, the stresses on that section would change if the elasticity modulus changes.
 
  • #11
If the strains and displacements are small, the changes in orientation of the plane and of the edges of the material elements are considered negligible. If the strains are large, we are dealing with non-linear material behavior, and you need to learn about the mathematics of large deformation behavior (google Cauchy-Green deformation tensor). If the displacements are large but the strains are small, this can be dealt with mathematically with the kinematics of the deformation, but with linear material behavior.
 

Similar threads

  • · Replies 6 ·
Replies
6
Views
1K
  • · Replies 69 ·
3
Replies
69
Views
5K
  • · Replies 1 ·
Replies
1
Views
3K
  • · Replies 3 ·
Replies
3
Views
4K
  • · Replies 2 ·
Replies
2
Views
2K
  • · Replies 6 ·
Replies
6
Views
1K
  • · Replies 1 ·
Replies
1
Views
2K
  • · Replies 1 ·
Replies
1
Views
3K
  • · Replies 35 ·
2
Replies
35
Views
4K
  • · Replies 4 ·
Replies
4
Views
2K