Problem 857
Question
Two wires of equal lengths are made of the same material wire A has a diameter that is twice as that of wire \(B\). If identical weights are suspended from the ends of these wires the increase in length is......... (A) Four times for wire \(\mathrm{A}\) as for wire \(\mathrm{B}\). (B) Twice for wire \(\mathrm{A}\) as for wire \(\mathrm{B}\). (C) Half for wire \(\mathrm{A}\) as for wire \(\mathrm{B}\). (D) One-fourth for wire \(\mathrm{A}\) as for wire \(\mathrm{B}\).
Step-by-Step Solution
Verified Answer
The increase in length for wire A is one-fourth that of wire B, which corresponds to option (D).
1Step 1: Identify the Young's modulus formula
Young's modulus (Y) is a measure of the stiffness of a material, and it is defined as the ratio of tensile stress to tensile strain. The formula for Young's modulus is given by:
\[Y = \frac{F/A}{\Delta L / L}\]
Where:
- Y is Young's modulus
- F is the applied force (weight)
- A is the cross-sectional area
- ΔL is the change in length
- L is the original length
2Step 2: Relate the diameter and cross-sectional area of the two wires
First, let's find the relationship between the cross-sectional areas of both wires. The cross-sectional area of a wire is given as:
\[A = \pi (\frac{d}{2})^{2}\]
Where d is the diameter of the wire.
Since wire A has a diameter twice the diameter of wire B:
\[d_{A} = 2 d_{B}\]
Now, we find the ratio of the cross-sectional areas of both wires.
\[\frac{A_{A}}{A_{B}} = \frac{\pi (\frac{d_{A}}{2})^{2}}{\pi (\frac{d_{B}}{2})^{2}}\]
3Step 3: Simplify the ratio of cross-sectional areas
Now, simplify the equation by substituting the relationship between the diameters:
\[\frac{A_{A}}{A_{B}} = \frac{\pi (\frac{2 d_{B}}{2})^{2}}{\pi (\frac{d_{B}}{2})^{2}}\]
\[\frac{A_{A}}{A_{B}} = \frac{d_{A}^2}{d_{B}^2} = \frac{(2d_{B})^2}{d_{B}^2} = 4\]
The cross-sectional area of wire A is 4 times larger than that of wire B.
4Step 4: Use the Young's modulus formula to compare the increase in length
We will use the Young's modulus formula to find the relationship between the increase in lengths for both wires. The wires are made of the same material, so their Young's modulus is the same. Since Y, F, and L are constant for both wires, we have:
\[\frac{A_{A}}{\Delta L_{A}} = \frac{A_{B}}{\Delta L_{B}}\]
Now, substitute the relationship of the cross-sectional areas and solve for the ratio of the increase in lengths:
\[\frac{4A_{B}}{\Delta L_{A}} = \frac{A_{B}}{\Delta L_{B}}\]
\[\frac{\Delta L_{A}}{\Delta L_{B}} = \frac{1}{4}\]
So, when identical weights are suspended from the ends of both wires, the increase in length for wire A is one-fourth that of wire B, which corresponds to option (D).
Key Concepts
Tensile StressCross-Sectional AreaTensile Strain
Tensile Stress
Imagine pulling on a rope tied to a heavy object. The force you apply is what creates tensile stress in the rope. Tensile stress is an important concept when studying the strength and behavior of materials under force. It refers to the force per unit area exerted on an object when it is stretched or pulled. For instance, if you have a string and you pull it with a force, the tensile stress is defined by the amount of force you are applying divided by the cross-sectional area of the string. The formula for tensile stress (σ) is:\[σ = \frac{F}{A}\]Where:
- \(σ\): Tensile stress (in Pascals)
- \(F\): Force applied (in Newtons)
- \(A\): Cross-sectional area (in square meters)
Cross-Sectional Area
The cross-sectional area of a wire gives us an insight into how large the wire is when we look "inside" it, across its cut surface. For a wire with a circular cross-section, this area is calculated using the formula for the area of a circle:\[A = \pi \left(\frac{d}{2}\right)^2\]Where:
- \(A\): Cross-sectional area (in square meters)
- \(d\): Diameter of the wire (in meters)
Tensile Strain
Tensile strain gives us a measure of how much a material stretches when a force is applied. It is the ratio of the change in length (ΔL) of a material to its original length (L). This is a dimensionless quantity and can be thought of as the relative elongation of the material.The formula for tensile strain (ε) is:\[ε = \frac{ΔL}{L}\]Where:
- \(ε\): Tensile strain (unitless)
- \(ΔL\): Change in length (in meters)
- \(L\): Original length (in meters)
Other exercises in this chapter
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