/*! 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 74 The \(50-\mathrm{mm}\) peephole ... [FREE SOLUTION] | 91Ó°ÊÓ

91Ó°ÊÓ

The \(50-\mathrm{mm}\) peephole of a large furnace operating at \(450^{\circ} \mathrm{C}\) is covered with a material having \(\tau=0.8\) and \(\rho=0\) for irradiation originating from the furnace. The material has an emissivity of \(0.8\) and is opaque to irradiation from a source at room temperature. The outer surface of the cover is exposed to surroundings and ambient air at \(27^{\circ} \mathrm{C}\) with a convection heat transfer coefficient of \(50 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Assuming that convection effects on the inner surface of the cover are negligible, calculate the heat loss by the furnace and the temperature of the cover.

Short Answer

Expert verified
The short answer for this problem is as follows: First, find the irradiation from the furnace using the Stefan-Boltzmann law with the given temperature and tau value. Then, calculate the total emissive power of the material using its emissivity and Stefan-Boltzmann constant. Set up the radiative and convective heat transfer equations, and combine them to get the total heat transfer equation. Finally, solve for the temperature of the cover and the heat loss by the furnace using a numerical method or software tool.

Step by step solution

01

Calculate the irradiation from the furnace

First, we need to calculate the irradiation from the furnace, \(I_{furnace}\). We use the Stefan-Boltzmann law: \[ I_{furnace} = \tau \cdot \sigma \cdot T_{furnace}^4 \] where \(\tau = 0.8\) is the transmissivity of the material, \(\sigma = 5.67 \cdot 10^{-8} \ \mathrm{W/m^2K^4}\) is the Stefan-Boltzmann constant, \(T_{furnace} = 450^{\circ}\mathrm{C} + 273.15 = 723.15\ \mathrm{K}\) is the furnace temperature in Kelvin. Now, we can solve for \(I_{furnace}\): \[ I_{furnace} = 0.8 \cdot 5.67 \cdot 10^{-8} \cdot (723.15)^4 \]
02

Calculate the total emissive power of the material

Next, we need to calculate the total emissive power of the material, \(E_{material}\). We use the formula: \[ E_{material} = \epsilon \cdot \sigma \cdot T_{material}^4 \] where \(\epsilon = 0.8\) is the emissivity of the material, \(T_{material}\) is the temperature of the cover in Kelvin.
03

Set up the radiative heat transfer equation

Now, we can set up the radiative heat transfer equation: \[ q_{rad} = AI_{furnace} - AE_{material} \] where \(A\) is the area of the peephole, which we will later cancel out.
04

Set up the convection heat transfer equation

We will now set up the convection heat transfer equation: \[ q_{conv} = hA(T_{material} - T_{ambient}) \] where \(h = 50\ \mathrm{W/m^2K}\) is the convection heat transfer coefficient, \(T_{ambient} = 27^{\circ}\mathrm{C} + 273.15 = 300.15\ \mathrm{K}\) is the ambient temperature.
05

Combine the radiative and convective heat transfer equations

The total heat transfer is the sum of the radiative and convective heat transfers: \[ q_{total} = q_{rad} + q_{conv} \] Substituting the expressions from Steps 3 and 4: \[ q_{total} = A(I_{furnace} - E_{material}) + hA(T_{material} - T_{ambient}) \] Since we are interested in the total heat loss and not per unit surface area, we can divide both sides by \(A\) and cancel it out: \[ \frac{q_{total}}{A} = I_{furnace} - E_{material} + h(T_{material} - T_{ambient}) \]
06

Solve for the temperature of the cover

Now we need to solve for \(T_{material}\). First, we plug in the expression for \(E_{material}\) from Step 2: \[ \frac{q_{total}}{A} = I_{furnace} - \epsilon \sigma T_{material}^4 + h(T_{material} - T_{ambient}) \] Solve this non-linear equation for \(T_{material}\) using a numerical method or software tool. Once you have \(T_{material}\), plug it back into both the radiative and convective equations to find \(q_{rad}\) and \(q_{conv}\). Finally, calculate the total heat loss \(q_{total}\).

Unlock Step-by-Step Solutions & Ace Your Exams!

  • Full Textbook Solutions

    Get detailed explanations and key concepts

  • Unlimited Al creation

    Al flashcards, explanations, exams and more...

  • Ads-free access

    To over 500 millions flashcards

  • Money-back guarantee

    We refund you if you fail your exam.

Over 30 million students worldwide already upgrade their learning with 91Ó°ÊÓ!

Key Concepts

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

Stefan-Boltzmann Law
When dealing with heat transfer, the Stefan-Boltzmann Law is crucial as it helps us calculate the amount of thermal radiation emitted by a surface. This law states that the power radiated by a black body per unit area is directly proportional to the fourth power of the black body's absolute temperature. Mathematically, it is expressed as:\[ E = \sigma T^4 \]where:
  • \(E\) is the emissive power
  • \(\sigma = 5.67 \times 10^{-8} \, \mathrm{W/m^2K^4}\) is the Stefan-Boltzmann constant
  • \(T\) is the absolute temperature of the body in Kelvin
The use of this law is demonstrated in calculating the irradiation from the furnace. You need the temperature in Kelvin to apply it, so remember to convert from Celsius or other units to Kelvin first.
Emissivity
Emissivity is a material property that measures how effectively a surface emits thermal radiation compared to an ideal black body, which has an emissivity of 1. Real-world objects have an emissivity value between 0 and 1.
  • An emissivity close to 1 means the material is a good emitter of radiation.
  • An emissivity close to 0 means the material emits very little thermal radiation.
In the exercise, the covering material of the furnace peephole has an emissivity of 0.8. This indicates it is quite effective in emitting the thermal radiation, though not as perfect as a theoretical black body. When performing calculations involving emissive power, it is crucial to adjust the Stefan-Boltzmann Law to account for emissivity. This adjustment is done by multiplying the original equation with the emissivity \(\epsilon\), like:\[ E_{material} = \epsilon \sigma T_{material}^4 \]This formula helps in determining the total power radiated by a real material.
Convection Heat Transfer
Convection is a mode of heat transfer that occurs in fluids. It involves the bulk movement of molecules within fluids (liquids and gases) and is a major way heat is transferred in atmospheres, oceans, and within our homes.In the exercise, convection affects the outer surface of the furnace cover. The surrounding air at \(27^{\circ} \mathrm{C}\) aids in transferring heat away from the cover. Convection can be calculated using:\[ q_{conv} = hA(T_{material} - T_{ambient}) \]where:
  • \(q_{conv}\) is the heat transfer rate due to convection
  • \(h = 50 \mathrm{W/m^2K}\) is the convection heat transfer coefficient
  • \(A\) is the area
  • \(T_{material}\) and \(T_{ambient}\) are the temperatures of the material and surroundings in Kelvin
Understanding convection is key to solving this problem as it involves determining how much heat is being lost from the furnace through the process of air movement around the cover.
Radiative Heat Transfer
Radiative heat transfer occurs when thermal energy is emitted by a body due to its temperature and travels away in the form of electromagnetic waves. Unlike conduction and convection, radiation does not need a medium and can occur in a vacuum.In this problem, the furnace and the environmental factors surrounding it engage in radiative heat transfer. To determine the transfer rate:\[ q_{rad} = AI_{furnace} - AE_{material} \]This equation accounts for:
  • Radiation emitted by the furnace surface
  • Radiation emitted by the material
The net radiation is the difference between what the material receives and what it emits. Combine it with convection to find overall heat loss, which reflects real-world scenarios where surfaces are constantly interacting with their environments through multiple types of heat transfer.

One App. One Place for Learning.

All the tools & learning materials you need for study success - in one app.

Get started for free

Most popular questions from this chapter

Square plates freshly sprayed with an epoxy paint must be cured at \(140^{\circ} \mathrm{C}\) for an extended period of time. The plates are located in a large enclosure and heated by a bank of infrared lamps. The top surface of each plate has an emissivity of \(\varepsilon=0.8\) and experiences convection with a ventilation airstream that is at \(T_{\infty}=27^{\circ} \mathrm{C}\) and provides a convection coefficient of \(h=20 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The irradiation from the enclosure walls is estimated to be \(G_{\text {wall }}=450 \mathrm{~W} / \mathrm{m}^{2}\), for which the plate absorptivity is \(\alpha_{\text {wall }}=0.7\). (a) Determine the irradiation that must be provided by the lamps, \(G_{\text {lamp. }}\). The absorptivity of the plate surface for this irradiation is \(\alpha_{\text {Lamp }}=0.6\). (b) For convection coefficients of \(h=15,20\), and \(30 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), plot the lamp irradiation, \(G_{\text {lamp, as a }}\) function of the plate temperature, \(T_{s}\), for \(100 \leq\) \(T_{x} \leq 300^{\circ} \mathrm{C}\). (c) For convection coefficients in the range from 10 to \(30 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) and a lamp irradiation of \(G_{\text {lmp }}=\) \(3000 \mathrm{~W} / \mathrm{m}^{2}\), plot the airstream temperature \(T_{x}\) required to maintain the plate at \(T_{x}=140^{\circ} \mathrm{C}\).

Two small surfaces, \(A\) and \(B\), are placed inside an isothermal enclosure at a uniform temperature. The enclosure provides an irradiation of \(6300 \mathrm{~W} / \mathrm{m}^{2}\) to each of the surfaces, and surfaces A and B absorb incident radiation at rates of 5600 and \(630 \mathrm{~W} / \mathrm{m}^{2}\), respectively. Consider conditions after a long time has elapsed. (a) What are the net heat fluxes for each surface? What are their temperatures? (b) Determine the absorptivity of each surface. (c) What are the emissive powers of each surface? (d) Determine the emissivity of each surface.

Four diffuse surfaces having the spectral characteristics shown are at \(300 \mathrm{~K}\) and are exposed to solar radiation. Which of the surfaces may be approximated as being gray?

A furnace with a long, isothermal, graphite tube of diameter \(D=12.5 \mathrm{~mm}\) is maintained at \(T_{f}=2000 \mathrm{~K}\) and is used as a blackbody source to calibrate heat flux gages. Traditional heat flux gages are constructed as blackened thin films with thermopiles to indicate the temperature change caused by absorption of the incident radiant power over the entire spectrum. The traditional gage of interest has a sensitive area of \(5 \mathrm{~mm}^{2}\) and is mounted coaxial with the furnace centerline, but positioned at a distance of \(L=60 \mathrm{~mm}\) from the beginning of the heated section. The cool extension tube serves to shield the gage from extraneous radiation sources and to contain the inert gas required to prevent rapid oxidation of the graphite tube. (a) Calculate the heat flux \(\left(\mathrm{W} / \mathrm{m}^{2}\right)\) on the traditional gage for this condition, assuming that the extension tube is cold relative to the furnace. (b) The traditional gage is replaced by a solid-state (photoconductive) heat flux gage of the same area, but sensitive only to the spectral region between \(0.4\) and \(2.5 \mu \mathrm{m}\). Calculate the radiant heat flux incident on the solid-state gage within the prescribed spectral region. (c) Calculate and plot the total heat flux and the heat flux in the prescribed spectral region for the solidstate gage as a function of furnace temperature for the range \(2000 \leq T_{f} \leq 3000 \mathrm{~K}\). Which gage will have an output signal that is more sensitive to changes in the furnace temperature?

Estimate the wavelength corresponding to maximum emission from each of the following surfaces: the sun, a tungsten filament at \(2500 \mathrm{~K}\), a heated metal at \(1500 \mathrm{~K}\), human skin at \(305 \mathrm{~K}\), and a cryogenically cooled metal surface at \(60 \mathrm{~K}\). Estimate the fraction of the solar emission that is in the following spectral regions: the ultraviolet, the visible, and the infrared.

See all solutions

Recommended explanations on Physics Textbooks

View all explanations

What do you think about this solution?

We value your feedback to improve our textbook solutions.

Study anywhere. Anytime. Across all devices.