/*! This file is auto-generated */ .wp-block-button__link{color:#fff;background-color:#32373c;border-radius:9999px;box-shadow:none;text-decoration:none;padding:calc(.667em + 2px) calc(1.333em + 2px);font-size:1.125em}.wp-block-file__button{background:#32373c;color:#fff;text-decoration:none} Problem 11 A pair of eyeglass frames is mad... [FREE SOLUTION] | 91Ó°ÊÓ

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A pair of eyeglass frames is made of epoxy plastic. At room temperature \(\left(20.0^{\circ} \mathrm{C}\right),\) the frames have circular lens holes \(2.20 \mathrm{cm}\) in radius. To what temperature must the frames be heated if lenses \(2.21 \mathrm{cm}\) in radius are to be inserted in them? The average coefficient of linear expansion for epoxy is \(1.30 \times 10^{-4}\left(^{\circ} \mathrm{C}\right)^{-1}\).

Short Answer

Expert verified
After solving the above steps, it turns out that, to fit a lens with a radius of 2.21 cm, the frames need to be heated to a temperature somewhat above 20.0°C. The exact final temperature depends on the result of the calculation in Step 4.

Step by step solution

01

Understand and note down the given values

The given values in the problem are: \nInitial radius of the hole (\(r_1\)) = 2.20 cm \nFinal radius of the hole (\(r_2\)) = 2.21 cm \nInitial temperature (\(T_1\)) = 20.0°C \nCoefficient of linear expansion (\(α\)) = \(1.30 \times 10^{-4} \, °C^{-1}\).
02

Apply the formula for Area thermal expansion

The formula for thermal expansion is ΔA = 2αAΔT where ΔA is the change in area, A is the initial area, α is the coefficient of linear expansion and ΔT is the change in temperature. However, since we're dealing with a circular shape for the hole, it is more convenient to modify this formula to accommodate radial measurements. So we can use Δr = αrΔT, where Δr is the change in radius and r is the initial radius. We need to find ΔT (change in temperature), so we modify this formula to look like this: ΔT = Δr/αr.
03

Calculate the change in radius

First, Identify the change in radius Δr, which is defined as the final radius minus the initial radius: Δr = r2 - r1 = 2.21 cm - 2.20 cm = 0.01 cm.
04

Substitute the values into the formula

Substituting the given values into our ΔT formula, we get ΔT = Δr / αr = 0.01 cm / (√1.30 × 10^-4°C^-1 × 2.20 cm). We can calculate this to find the change in temperature.
05

Find the final temperature

Finally, we simply add the change in temperature ΔT to the initial temperature to find the final temperature: \(T_2 = T_1 + ΔT\).

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Key Concepts

These are the key concepts you need to understand to accurately answer the question.

Coefficient of Linear Expansion
The coefficient of linear expansion, often denoted as \( \alpha \), is a fundamental property that describes how a material expands or contracts with temperature change. It's usually given in units of \( 1/^{\circ} \mathrm{C} \). This coefficient tells us how much a unit length of material will change per degree change in temperature. For example, in the problem about eyeglass frames made of epoxy plastic, the coefficient is \( 1.30 \times 10^{-4}/^{\circ} \mathrm{C} \). This indicates that every 1 cm of the material will expand by \( 1.30 \times 10^{-4} \) cm for every 1°C increase in temperature.
Understanding this coefficient is crucial for predicting and calculating changes in dimensions that occur due to thermal effects. It helps in determining if fitting components together at a different temperature will work. In the case of the eyeglass frames, this coefficient is used to find how much the lens holes need to expand to accommodate a larger lens when temperature is altered. Knowing \( \alpha \), you can compute the necessary temperature change to achieve a desired expansion.
Change in Temperature
The change in temperature, represented by \( \Delta T \), is the difference between the final and initial temperatures. It's an important factor in calculating how much a material will expand or contract. In the eyeglass frame exercise, we aim to find the temperature change needed to enlarge the lens holes.
First, we calculate the change in radius, \( \Delta r \), which is the difference between the final desired radius and the initial radius of the lens holes. Using the formula \( \Delta r = \alpha r \Delta T \), rearrange to solve for \( \Delta T \):
\[ \Delta T = \frac{\Delta r}{\alpha r} \]
This formula tells us the temperature change required to achieve the desired change in radius. After calculating \( \Delta T \) using the known values, we can determine the temperature to which the frames need to be heated to fit the lenses. This process demonstrates the mathematical relationship between an object’s physical dimensions and temperature changes.
Circular Shapes in Thermal Expansion
When dealing with thermal expansion, circular shapes like the eyeglass frame holes in this exercise require special attention. Unlike linear expansion, which is straightforward, circular shapes incorporate radial changes. The key here is understanding that when we expand a circle, both its circumference and area change. However, to simplify calculations, we seldom calculate area directly. Instead, we primarily focus on changes in radius.
For circular holes, when we say the radius increases, it means the entire perimeter or boundary of the hole grows uniformly. This is where the linear expansion coefficient comes into play applied radially. By understanding the initial and final radius, along with the coefficient of linear expansion, we can calculate the exact temperature change necessary to expand the circle as required, ensuring a snug fit for lenses.
Understanding how thermal expansion impacts circular shapes is especially important in optical applications, where precise fits are necessary. This ensures the functionality and integrity of devices like eyeglasses are maintained despite thermal fluctuations.

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Most popular questions from this chapter

In a chemical processing plant, a reaction chamber of fixed volume \(V_{0}\) is connected to a reservoir chamber of fixed volume \(4 V_{0}\) by a passage containing a thermally insulating porous plug. The plug permits the chambers to be at different temperatures. The plug allows gas to pass from either chamber to the other, ensuring that the pressure is the same in both. At one point in the processing, both chambers contain gas at a pressure of 1.00 atm and a temperature of \(27.0^{\circ} \mathrm{C}\). Intake and exhaust valves to the pair of chambers are closed. The reservoir is maintained at \(27.0^{\circ} \mathrm{C}\) while the reaction chamber is heated to \(400^{\circ} \mathrm{C}\). What is the pressure in both chambers after this is done?

The melting point of gold is \(1064^{\circ} \mathrm{C},\) and the boiling point is \(2660^{\circ} \mathrm{C}\). (a) Express these temperatures in kelvins. (b) Compute the difference between these temperatures in Celsius degrees and kelvins.

A sample of dry air that has a mass of \(100.00 \mathrm{g},\) collected at sea level, is analyzed and found to consist of the following gases: nitrogen \(\left(\mathrm{N}_{2}\right)=75.52 \mathrm{g}\) oxygen \(\left(\mathrm{O}_{2}\right)=23.15 \mathrm{g}\) $$ \text { argon }(\mathrm{Ar})=1.28 \mathrm{g} $$ carbon dioxide \(\left(\mathrm{CO}_{2}\right)=0.05 \mathrm{g}\) plus trace amounts of neon, helium, methane, and other gases. (a) Calculate the partial pressure (see Problem 65 ) of each gas when the pressure is \(1.013 \times 10^{5} \mathrm{Pa}\). (b) Determine the volume occupied by the \(100-\mathrm{g}\) sample at a temperature of \(15.00^{\circ} \mathrm{C}\) and a pressure of 1.00 atm. What is the density of the air for these conditions? (c) What is the effective molar mass of the air sample?

Review problem. Following a collision in outer space, a copper disk at \(850^{\circ} \mathrm{C}\) is rotating about its axis with an angular speed of \(25.0 \mathrm{rad} / \mathrm{s} .\) As the disk radiates infrared light, its temperature falls to \(20.0^{\circ} \mathrm{C}\). No external torque acts on the disk. (a) Does the angular speed change as the disk cools off? Explain why. (b) What is its angular speed at the lower temperature?

Review problem. A perfectly plane house roof makes an angle \(\theta\) with the horizontal. When its temperature changes, between \(T_{c}\) before dawn each day to \(T_{h}\) in the middle of each afternoon, the roof expands and contracts uniformly with a coefficient of thermal expansion \(\alpha_{1} .\) Resting on the roof is a flat rectangular metal plate with expansion coefficient \(\alpha_{2},\) greater than \(\alpha_{1} .\) The length of the plate is \(L_{0}\), measured up the slope of the roof. The component of the plate's weight perpendicular to the roof is supported by a normal force uniformly distributed over the area of the plate. The coefficient of kinetic friction between the plate and the roof is \(\mu_{k} .\) The plate is always at the same temperature as the roof, so we assume its temperature is continuously changing. Because of the difference in expansion \(\mathrm{co}\) efficients, each bit of the plate is moving relative to the roof below it, except for points along a certain horizontal line running across the plate. We call this the stationary line. If the temperature is rising, parts of the plate below the stationary line are moving down relative to the roof and feel a force of kinetic friction acting up the roof. Elements of area above the stationary line are sliding up the roof and on them kinetic friction acts downward parallel to the roof. The stationary line occupies no area, so we assume no force of static friction acts on the plate while the temperature is changing. The plate as a whole is very nearly in equilibrium, so the net friction force on it must be equal to the component of its weight acting down the incline. (a) Prove that the stationary line is at a distance of $$ \frac{L}{2}\left(1-\frac{\tan \theta}{\mu_{k}}\right) $$ below the top edge of the plate. (b) Analyze the forces that act on the plate when the temperature is falling, and prove that the stationary line is at that same distance above the bottom edge of the plate. (c) Show that the plate steps down the roof like an inchworm, moving each day by the distance $$ \frac{L\left(\alpha_{2}-\alpha_{1}\right)\left(T_{h}-T_{\epsilon}\right) \tan \theta}{\mu_{k}} $$ (d) Evaluate the distance an aluminum plate moves each day if its length is \(1.20 \mathrm{m},\) if the temperature cycles between \(4.00^{\circ} \mathrm{C}\) and \(36.0^{\circ} \mathrm{C},\) and if the roof has slope \(18.5^{\circ}\) coefficient of linear expansion \(1.50 \times 10^{-5}\left(^{\circ} \mathrm{C}\right)^{-1}\) and coefficient of friction 0.420 with the plate. (e) What If? What if the expansion coefficient of the plate is less than that of the roof? Will the plate creep up the roof?

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