How Do Material Properties Affect Wire Deformation?

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The discussion focuses on calculating the stress, strain, extension, and elastic energy stored in a copper wire and a carbon fiber wire under a suspended mass. For the copper wire, with a Young's modulus of 130 Pa, the stress is calculated as 25 kPa, resulting in a strain of 0.0052 and an extension of 1.04 cm. In contrast, the carbon fiber, with a Young's modulus of 7500 GPa, shows significantly lower strain and extension values due to its higher stiffness, resulting in an extension of only 0.801 nm. Participants clarify calculations and correct errors throughout the discussion, emphasizing the importance of unit consistency. The thread highlights the significant differences in material properties and their effects on wire deformation.
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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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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:
 
Hay tT:
Ahhh! Silly me :redface:

strain = 130/25000 = 0.0052
 
™ … 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
 
lemon said:
Ahhh! Silly me :redface:

Too much stress and strain! :biggrin:
 
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?
 
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:
 
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
 
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
 
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