How Do Material Properties Affect Wire Deformation?

In summary: Ep=1/2FΔx=1/2(10)(8.01x10-10)=4.005x10-9J, or 0.004005nJIn summary, we calculated the stress, strain, extension, and elastic energy stored for a copper wire with length 200cm, radius 0.40mm, mass of 1.00kg, and Young modulus of 130Pa. We also repeated the calculations for the case of a carbon fibre with Young modulus 7500GPa.
  • #1
lemon
200
0
1. A copper wire has length 200cm and radius 0.40mm. A mass of 1.00kg is suspended from the end and allowed to come to rest. The Young modulus of copper is 130Pa. Calculate:
a) the stress
b) the strain
c) the extension
d) the elastic energy stored
Repeat the calculations for the case of a carbon fibre of Young modulus 7500GPa.
2. stress=F/A
strain=deltax/L
E=stress/strain
let gravity=-10m/s
let deltax = ^x

3.
a) F = 1.0kg x 10m/s = 10N
Stress = 10/π0.00042=25000Pa, 25kPa

b) Now I'm already stuck because I don't have ^x to calculate the strain.
 
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  • #2
Hi lemon! :smile:

(have a delta: ∆ :wink:)
lemon said:
1. A copper wire has length 200cm and radius 0.40mm. A mass of 1.00kg is suspended from the end and allowed to come to rest. The Young modulus of copper is 130Pa. Calculate:
a) the stress
b) the strain

2. stress=F/A
strain=deltax/L
E=stress/strain

Stress = 10/π0.00042=25000Pa, 25kPa

b) Now I'm already stuck because I don't have ^x to calculate the strain.

(oooh … correct homework template, but without the clutter i like it! :biggrin:)

I don't understand … you have the stress, and you have E = stress/strain …

what am i missing? :redface:
 
  • #3
Hay tT:
Ahhh! Silly me :redface:

strain = 130/25000 = 0.0052
 
  • #4
™ … for copying-and-pasting … ™
π²³ ∞ ° → ~ µ ρ σ τ ω ∑ … √ ∫ ≤ ≥ ± ∃ · θ φ ψ Ω α β γ δ ∂ ∆ ∇ ε λ Λ Γ ô
see also Redbelly98's "useful stuff" list

Thank you
 
  • #5
lemon said:
Ahhh! Silly me :redface:

Too much stress and strain! :biggrin:
 
  • #6
ok. So if I haven't made anymore silly mistakes:

For the Copper wire:
F=10N
Stress=25kPa
Strain=0.0052
Δx=0.0052x2.0m = 0.0104m
Ep=1/2x10x0.0104 = 0.052J

For the Carbon fibre:
F=10N
Stress=25kPa
Strain=25/(7500x109) = 3.3x10-9
Δx=(3.3x10-9)x2.0=6.6x10-9
Ep=1/2x10x(6.6x10-9)=33x10-9J

How'd I do?
 
  • #7
Hi lemon ! :smile:

Fine, except that for the copper, you seem to have used E = strain/stress, and I think if the original length is given in cm, you should give the extension in cm also (well, maybe only for the copper). :wink:
 
  • #8
tiny-tim Hi lemon !

Fine, except that for the copper, you seem to have used E = strain/stress

I haven't calculated for Young's modulus in this question tT. Not sure I understand.


and I think if the original length is given in cm, you should give the extension in cm also (well, maybe only for the copper).

Copper: Δx=0.0052x2.0m = 0.0104m = 1.04cm
Carbon fibre: Δx=(3.3x10-9)x2.0=6.6x10-9m
 
  • #9
errr! I have just recalculated - not sure if my calculator has a problem suddenly but when I calculate the stress I get:
10N/∏x0.0004²=19894367.89

What's going on here?
 
  • #10
ok I have to say sorry sorry sorry to everyone.
did some bum calculations there.

I have hopefully recalculated correctly.

a) F=1.0kg x 10m/s = 10N
δ=10/∏0.00042=19894367.89 or 20x106 (2s.f.) or 20.0MPa

b) E=δ/ε. ε=δ/E, Young's modulus
20.0MPa/130GPa=1.5x10-4 (2s.f.)

c) Δx=εxL. 1.5x10-4x2.0m=3x10-4m, or 0.0003cm

d) Ep=1/2FΔx=1/2(10)(3x10-4m)=1.5x10-3J

Would somebody be good enough to see if I have finally got my head straight please
 
  • #11
Looks ok! :smile:

(except the decimal point in the cm :wink:)
 
  • #12
ooopppss!:redface:
c) Δx=εxL. 1.5x10-4x2.0m=3x10-4m, or 0.0003m
or 0.03cmo:)
 
  • #13
Repeat the calculations for the case of a carbon fibre of Young modulus 7500GPa.

F=10N
δ=20.0MPa
E=7500GPa

E=20.0MPa/7500GPa=2.67x10-6

Δx=(2.67x10-6)x(3x10-4)=8.01x10-10m
0.801nm, or 80.1ncm
 

1. What is the difference between stress and strain?

Stress is the amount of force applied to a material, while strain is the resulting deformation or change in shape of the material. Stress and strain are directly related, with strain being a measure of how a material responds to stress.

2. What are the different types of stress?

There are three main types of stress: tensile stress, compressive stress, and shear stress. Tensile stress occurs when a material is being pulled apart, compressive stress occurs when a material is being pushed together, and shear stress occurs when a material is being twisted or cut.

3. How does stress affect materials?

Stress can cause materials to deform, break, or change in other ways. Too much stress can lead to failure or structural damage, while controlled stress can be beneficial for shaping and strengthening materials.

4. What factors influence the amount of strain in a material?

The amount of strain in a material is influenced by its elastic properties, the type and amount of applied stress, and the material's temperature. Different materials have different levels of elasticity, which affects how they respond to stress.

5. How is stress and strain measured?

Stress is typically measured in units of force per unit area, such as pounds per square inch (psi) or newtons per square meter (Pa). Strain is measured as the change in length or dimension of a material divided by its original length or dimension, expressed as a percentage or decimal. Both stress and strain can be measured using specialized instruments or calculated using known formulas.

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