Young's modulus problem - need a hint

In summary, the problem involves two wires, one brass and one copper, connected to form a 1m length. A force is applied, resulting in a total length change of 0.5 mm. Using Hooke's law and compatibility of deformations, it is possible to find the amount of length change in each section of the wire, given their respective Young's moduluses. The solution involves setting up and solving three equations with three unknowns, resulting in an increase of 0.21 mm for the brass wire.
  • #1
redshift
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Young's modulus problem -- need a hint

There are two wires, one brass the other copper, both 50 cm long and 1.0 mm diameter. They are somehow connected to form a 1m length. A force is applied to both ends, resulting in a total length change of 0.5 mm. Given the respective young's moduluses of 1.3 x 10^11 and 1.0 x 10^11, I'm supposed to find the amount of length change in each section.

Apparently a variation of Hooke's law should be used here, such as F/A=Y(change in length/original length)

I'm stuck on how can I solve this with 2 unknowns (force and change in length)?
Regards
 
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  • #2
redshift said:
There are two wires, one brass the other copper, both 50 cm long and 1.0 mm diameter. They are somehow connected to form a 1m length. A force is applied to both ends, resulting in a total length change of 0.5 mm. Given the respective young's moduluses of 1.3 x 10^11 and 1.0 x 10^11, I'm supposed to find the amount of length change in each section.

Apparently a variation of Hooke's law should be used here, such as F/A=Y(change in length/original length)

I'm stuck on how can I solve this with 2 unknowns (force and change in length)?
Regards

Hello redshift! I'm going to rewritte your problem in terms of stress [tex]\sigma[/tex] (Pa) and unitary deformation [tex]\epsilon=\frac{L-L_o}{L_o}[/tex] where Lo is the original lenght. So that, the stress exerted is the same in each section of the wire:

Hooke's law: [tex] \sigma=E_t \epsilon_t=E_1 \epsilon_1=E_2 \epsilon_2[/tex] where "Et" (N/m^2) is the apparent Young modulus of the complete wire.

Compatibility of deformations: [tex]\bigtriangleup L=\bigtriangleup L_1 + \bigtriangleup L_2[/tex]


Then, you have three equations for three unknowns: Et, epsilon1 and epsilon2.

Hope this help you a bit.




You've got two unknowns for
 
  • #3
Many thanks

I think I get it. Based on your equations, the ratio of the young's moduluses should equal the ratio of the individual increases, that is, 13/10 = L1/L2
Therefore, 10L1 = 13L2
Since, L1 = L2 = 0.5, then L1 = 0.5 - L2. Plugging this into the above gives 10(0.5 - L2) = 13L2, so that the increase of L2 (brass wire) is 0.21 mm.

Many thanks!
 

FAQ: Young's modulus problem - need a hint

What is Young's modulus?

Young's modulus, also known as the modulus of elasticity, is a measure of a material's stiffness or ability to resist deformation under an applied force. It is denoted by the letter E and has units of pressure or stress.

How is Young's modulus calculated?

Young's modulus is calculated by dividing the stress (force per unit area) by the strain (change in length divided by original length) of a material. It is typically expressed in units of gigapascals (GPa) or megapascals (MPa).

What does a high or low Young's modulus indicate?

A high Young's modulus indicates that a material is stiff and difficult to deform, while a low Young's modulus indicates that a material is more flexible and easier to deform. Materials with high Young's moduli are often used in structural applications, while those with low Young's moduli are used in applications where flexibility is desired.

What factors influence Young's modulus?

The Young's modulus of a material is influenced by its composition, structure, and temperature. Generally, materials with strong chemical bonds and ordered, crystalline structures have higher Young's moduli, while materials with weaker bonds and more disordered structures have lower Young's moduli.

Why is Young's modulus important in materials science?

Young's modulus is an important property in materials science as it helps engineers and scientists understand and predict how materials will behave under stress and strain. It is also used in the design and testing of structures and materials for various applications, such as in construction, manufacturing, and biomedical fields.

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