How Does Inflation Affect the Thickness of a Plastic Ball?

In summary, the conversation discussed the problem of finding the thickness of a plastic ball after inflation, given initial thickness, tangential stresses, and modulus of elasticity values. The solution involved using Hooke's Law, normal stress and strain equations, and generalized Hooke's Law to derive the transverse strain. The final answer was found to be 1.1997 mm.
  • #1
hatchelhoff
65
0

Homework Statement



A plastic ball is inflated enough to produce tangential stresses. σX = σY = 2000Kpa
The radial thickness of the material is 1.2mm brfore inflation. Find the thickness after inflation if the tensile modulus of elasticity is 3.4Gpa and the shear modulus is 1.4Gpa.


Homework Equations


σ = Stress, ε= Strain, E = Modulus of Elasticity, G = Shear Modulus. v = Poisons Ratio

σ = F/A, ε = Elongation/Origional Length, σ = Modulus of Elasticity x ε
Elongation = (Force x Length) / (AE), v = -Lateral Strain/axial Strain
E = 2G(1 + v), ε1 = σ1/E - vσ2/E, σ1 = (E(ε1 + vε2))/(1-vxv)


The Attempt at a Solution


E = 2G(1 + v)
v = (E-2G)/2G
v = 0.2143

ε1 = σ1/E - vσ2/E
ε1 = 0.00046

ε = Elongation/Origional Length
Elongation = ε x Origional Length
= 0.00046 x 1.2
 
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  • #2
Everything you have matches what I have so far.

For your final answer, remember that since the ball is expanding, the cross-sectional area of the ball is also increasing. Based on Hooke's Law, normal stress, and normal strain equations, you can derive a mathematical relationship between thickness t and the cross-sectional area, A.

σ=εE, σ=P/A, and ε=(L-t_i)/t_i (t_i = initial thickness)

Therefore: [(L/t_1)-1]*E=P/A

Since there is an inverse relationship between t and A, and you know that A is increasing, we know that is decreasing. This means that for this problem, your final t value must be smaller than your initial t value.

Thus, t_final = t_i - L
 
  • #3
hatchelhoff: (1) The unit symbol for kilopascal is spelled kPa, not Kpa. Uppercase K means kelvin, and lowercase p means pico. The unit symbol for gigapascal is spelled GPa, not Gpa. Always use correct capitalization of units and prefixes.

(2) Always leave a space between a numeric value and its following unit symbol. E.g., 1.2 mm, not 1.2mm. See the international standard for writing units (ISO 31-0).

(3) Try to avoid using the letter "x" for the multiplication operator, because it cannot necessarily be distinguished from the variable x. Usually use an asterisk (*), instead.

(4) Two quantities multiplied together must be separated by an asterisk, middle dot (·), space, or parentheses. E.g., v*sigma2, not vsigma2.

(5) For exponentiation, use the caret (^) symbol. E.g., v^2, instead of v*v.

(6) Generally always maintain at least four significant digits throughout all your intermediate calculations, then round only the final answer to three significant digits, unless the first significant digit of the final answer is 1, in which case round the final answer to four significant digits.

(7) I did not understand post 2 yet, because L is undefined.

(8) hatchelhoff, I currently get a different answer from your current thickness answer in post 1. In post 1, it appears you are currently pretending there is strain in only one in-plane direction, which is not the case. I think you might be able to use generalized Hooke's law to derive the transverse (out-of-plane) strain. Give it a try.

(9) Also, I currently do not know why you are computing a transverse strain in post 1 with no Poisson effect. It does not seem to make sense yet.

(10) We are not allowed to give you the relevant equations for your homework, nor tell you how to solve your homework problem. We can only check your math. Keep trying.
 
Last edited:
  • #4
I forgot to define L as elongation, or the change in thickness.
 
  • #5
Thanks gOest. I agree with your logic that the Thickness must be less as the pressure increases. But according to the book I am using the thickness after inflation is 1.9 mm
 
  • #6
Thanks very much for your comments nvn
 
  • #7
hatchelhoff: If the answer in the book is 1.9 mm, then the book answer is wrong. Hint 1: Use generalized Hooke's law to compute eps1 and eps2. Hint 2: Using generalized Hooke's law again, add the three equations of generalized Hooke's law together, to derive eps3.

By the way, even though the general rule in item 6 of post 3 is to maintain at least four significant digits, strains are an exception. Because strains are so small, I usually maintain at least six significant digits throughout all strain calculations, then round the final answer to four or five significant digits.
 
Last edited:
  • #8
What do you mean by eps
 
  • #9
eps means epsilon.
 
  • #10
I have now calculated [itex]\epsilon[/itex]1 and [itex]\epsilon[/itex]2 and [itex]\epsilon[/itex]3 using the following equations
[itex]\epsilon[/itex]1 = ([itex]\sigma[/itex]1/E) -(v.[itex]\sigma[/itex]2/E)

[itex]\epsilon[/itex]2 = ([itex]\sigma[/itex]2/E) -(v.[itex]\sigma[/itex]1/E)

[itex]\epsilon[/itex]3 = v.([itex]\sigma[/itex]1/E) - v.([itex]\sigma[/itex]2/E)
There fore
[itex]\epsilon[/itex]1 = 4.6*10^-4
[itex]\epsilon[/itex]2 = 4.6*10^-4
[itex]\epsilon[/itex]3 = -7.14*10^-4

I am not sure what the next step is.
 
  • #11
hatchelhoff: Are you missing a negative sign in your third equation? Try again. Ignore hint 2 in post 7; although hint 2 is not wrong, it does not make sense here, and is not needed. Please see item 6 in post 3 (and see the second paragraph of post 7). Afterwards, the next step is to compute the final thickness of the plastic.
 
  • #12
Thanks nvn. I was missing a Minus sign in the equation for ε3
the new value is
ε3 = -2.52116*10^-4.

Im not sure how to deal with these strains which I have calculated.
Can I just simply add them together to find a total strain, and feed this total into a an equation
to find the thickness.
 
  • #13
hatchelhoff said:
Can I just simply add them together to find a total strain.

No, you now have eps3. Therefore, feed it into an equation to find the final thickness.
 
  • #14
Thanks nvn. Why did you choose ε1 as opposed to ε2 or ε3?
 
  • #15
hatchelhoff: I did not choose eps1.
 
  • #16
Sorry, I ment to say eps 3
 
  • #17
hatchelhoff: I chose eps3 because eps3 is in the direction perpendicular to the plate or surface.
 
  • #18
Thanks nvn
Here is my final solution
ε = L*ti/ti
L = ti + ti*ε
L = 1.2 mm + 1.2 mm * -2.52116 *10^-4
L= 1.1997 mm
 
  • #19
hatchelhoff: In post 18, your first equation is wrong, but your other two equations are correct, and your answer is correct.
 
  • #20
Thats great. Thanks very much nvn
 

1. What is the concept of stress and strain in materials?

Stress is the force applied to a material per unit area, while strain is the resulting deformation or change in shape of the material. Both stress and strain are important factors in determining the mechanical properties of a material.

2. What is the relationship between stress and strain?

The relationship between stress and strain is described by stress-strain curves, which show how a material responds to applied stress. This relationship can vary depending on the type of material and its composition.

3. How does the structure of a material affect its stress-strain relationship?

The structure of a material, including factors such as grain size and shape, can significantly affect its stress-strain relationship. For example, materials with smaller grain sizes tend to have higher strength and stiffness.

4. What are the different types of stress-strain relationships?

There are three main types of stress-strain relationships: elastic, plastic, and viscoelastic. In an elastic material, stress and strain are directly proportional, while in a plastic material, the relationship is nonlinear. Viscoelastic materials have a time-dependent stress-strain relationship.

5. How is the stress-strain relationship used in materials testing and design?

The stress-strain relationship is an important tool in materials testing and design. It allows scientists and engineers to determine the mechanical properties of a material, such as its strength and stiffness, and to predict how it will behave under different loading conditions. This information is crucial in selecting suitable materials for various applications.

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