Derivation of normal strain

In summary, the source authors are using a more complicated calculation to approximate length(ab) as its horizontal projection, but this more complicated calculation may not be valid for all cases.
  • #1
nissan4l0
11
0
http://imgur.com/SnHyP

What are the mathematical steps and assumptions to reach the conclusion that length(ab) ≈ dx + ∂u/∂x*dx ?

If you consider the the squares of the gradients to be negligible, you still have a square root and multiplication by the constant "2". What other assumptions do we make to derive the final equation?

*Edit, I should have posted this in calculus, I apologize.
 
Last edited:
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  • #2
You were right to post this in engineering : it is an engineering issue.

The statement

[tex]{\rm{length(ab)}} = \sqrt {{{\left( {dx + \frac{{\partial {u_x}}}{{\partial x}}dx} \right)}^2} + {{\left( {\frac{{\partial {u_y}}}{{\partial x}}dx} \right)}^2}} [/tex]

is nothing more than pythagoras theorem for the horizontal and vertical components of ab.
I assume you are comfortable with this.

Now AB was originally horizontal and it is stated that the strain is very small. Thus the angles alpha and beta in the diagram are very small.

If beta is very small then the hypotenuse (ab) is very nearly the same as the horizontal component, which is


[tex]dx + \frac{{\partial {u_x}}}{{\partial x}}dx[/tex]


Thus

[tex]{\rm{length(ab)}} \approx dx + \frac{{\partial {u_x}}}{{\partial x}}dx[/tex]
 
  • #3
OP, I think your question is simply: how did they go from:

[itex]length(ab)= \sqrt{\left(dx+\frac{\partial u_x}{\partial x}dx\right)^2+\left(\frac{\partial u_y}{\partial x}dx\right)^2}[/itex]

to

[itex]length(ab)\approx dx+\frac{\partial u_x}{\partial x}dx[/itex] ?


The math doesn't work, I agree.

From a geometric point-of-view, as Studiot suggested, they assume that [itex]length(ab)[/itex] is equal to its horizontal projection, for small deformations.


However, I'm not sure that I buy that, to be honest.



In terms of the actual physics, and in looking at the provided diagram, I can tell you that if it were only a simple shear, you could get the angle change [itex]\alpha + \beta[/itex] but there has to be some sort of homogeneous (axial) deformation in order for BOTH [itex]dx[/itex] and [itex]dy[/itex] to change lengths.

For example, one way to arrive at the apparent deformed shape would be:

1) apply a homogenous deformation (e.x. to the right, of magnitude ([itex]length(ab)-dx[/itex]) -- i.e. [itex]\sqrt{\left(dx+\frac{\partial u_x}{\partial x}dx\right)^2+\left(\frac{\partial u_y}{\partial x}dx\right)^2}-dx[/itex])

2) apply a simple shear (e.x. to the right, of amount [itex]\alpha + \beta[/itex])

3) apply a rigid body rotation (e.x. counter-clockwise, of amount [itex]\alpha[/itex])

Does that make sense?



You can play with this though.

Take 1) to be zero. No deformation to the right means [itex]length(ab)=dx[/itex].

2) and 3) still apply - and so we have a simple shear and a rigid body rotation.

We should still get [itex]length(ab)=dx[/itex] in this case under either a small shear or a large shear. However, due to the rigid body rotation, [itex]\frac{\partial u_x}{\partial x}dx[/itex] in their diagram would be nonzero and so their expression [itex]length(ab)\approx dx+\frac{\partial u_x}{\partial x}dx[/itex] is not equal to [itex]dx[/itex]. This doesn't mean that they are wrong, but I cannot immediately justify approximating [itex]length(ab)[/itex] as its horizontal projection, for the general case that they are showing.

In other words, I don't like their expression [itex]length(ab)\approx dx+\frac{\partial u_x}{\partial x}dx[/itex] unless someone can prove to me that it agrees with more advanced solid mechanics.
 
  • #4
OP, I think your question is simply: how did they go from:

...

to

...

I thought this at first but came to the conclusion that the source material authors were simply replacing or substituting a simpler calculation, not simplyfying a more complicated one.

This is not unusual, for instance the substitution of the chord for the arc or the other way in circular calculations of small angle.

We will not know more without more information from the source.
 

1. What is normal strain?

Normal strain is a measure of the change in length of a material per unit length due to an applied force or stress.

2. How is normal strain calculated?

Normal strain is calculated by taking the change in length of a material and dividing it by its original length. This can be expressed as ΔL/L, where ΔL is the change in length and L is the original length.

3. What is the difference between normal strain and shear strain?

Normal strain is a measure of the change in length of a material along its longitudinal axis, while shear strain is a measure of the change in shape of a material due to an applied force parallel to its surface. Normal strain causes a material to elongate or compress, while shear strain causes a material to deform or twist.

4. How does normal strain affect the properties of a material?

The magnitude of normal strain can affect the strength, stiffness, and ductility of a material. Higher levels of normal strain can cause a material to become weaker and less stiff, while lower levels of normal strain can make a material more ductile and able to withstand larger amounts of stress.

5. What are some real-world applications of normal strain?

Normal strain is a crucial concept in engineering, as it is used to design and analyze structures and materials. It is also important in fields such as geology and biology, where it is used to study the behavior of rocks and living tissues under stress.

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