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An electric heater with the total surface area of \(0.25 \mathrm{~m}^{2}\) and emissivity \(0.75\) is in a room where the air has a temperature of \(20^{\circ} \mathrm{C}\) and the walls are at \(10^{\circ} \mathrm{C}\). When the heater consumes \(500 \mathrm{~W}\) of electric power, its surface has a steady temperature of \(120^{\circ} \mathrm{C}\). Determine the temperature of the heater surface when it consumes \(700 \mathrm{~W}\). Solve the problem (a) assuming negligible radiation and (b) taking radiation into consideration. Based on your results, comment on the assumption made in part ( \(a\) ).

Short Answer

Expert verified
1. In part (a), we neglect radiation. Calculate the heater surface temperature (T2) in this case by using the relationship: \(T_2 = T_\text{air} + \frac{P_2}{P_1} (T_1 - T_\text{air})\) 2. In part (b), we consider radiation. Solve the equation numerically to find the value of T2: \(P_2 = K (T_2 - T_\text{air}) + \epsilon \sigma A (T_2^4 - T_\text{wall}^4)\) 3. Compare the results obtained in parts (a) and (b) and comment on the differences in surface temperatures.

Step by step solution

01

Part (a): Neglecting Radiation

Let's start by analyzing the situation when we assume negligible radiation. In this case, 100% of the delivered power (P) is dedicated to heating the room's air. From the steady-state situation, we can establish a relationship between temperature and power consumption: \(P_1 = K (T_1 - T_\text{air})\) Here, K is a constant representing the heat transfer from the heater's surface to the air. Since we don't take into account the radiation, the value of K should remain constant when the power consumption increases. Now, we can use the same relationship for the problem scenario: \(P_2 = K (T_2 - T_\text{air})\) From these two relationships, we can find T2: \(\frac{P_1}{P_2} = \frac{T_1 - T_\text{air}}{T_2 - T_\text{air}}\) Solve for T2: \(T_2 = T_\text{air} + \frac{P_2}{P_1} (T_1 - T_\text{air})\) Finally, plug in the given values to determine T2.
02

Part (b): Considering Radiation

Now we will take radiation into account. The Stefan-Boltzmann law helps us determine the power radiated from the heater's surface. The Stefan-Boltzmann law states that the radiated power is given by: \(P_\text{rad} = \epsilon \sigma A (T^4 - T_\text{wall}^4)\) where \(\sigma\) is the Stefan-Boltzmann constant: \(5.67 \times 10^{-8} \mathrm{W m^{-2} K^{-4}}\). As the heat given to the room's air is now decreased, we have: \(P_\text{air} = P - P_\text{rad}\) The relationships between power, temperature, and radiation can be established for the steady-state case and the problem scenario: For the initial steady-state case: \(P_1 = K (T_1 - T_\text{air}) + \epsilon \sigma A (T_1^4 - T_\text{wall}^4)\) For the problem scenario: \(P_2 = K (T_2 - T_\text{air}) + \epsilon \sigma A (T_2^4 - T_\text{wall}^4)\) There is no closed-form analytical solution for T2 in this case, so we need to solve the above equation numerically using a numerical method such as the Newton-Raphson method or a root-finding algorithm. Then, compare the results obtained in parts (a) and (b) and comment based on the differences in surface temperatures.

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Key Concepts

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

Stefan-Boltzmann Law
Understanding the Stefan-Boltzmann Law is foundational when studying heat transfer, particularly radiation. This law reveals how the amount of radiant energy emitted from a black body in space is proportional to the fourth power of the black body's temperature. Mathematically, it's represented as:
\[P_{\text{rad}} = \epsilon \sigma A (T^4 - T_{\text{environment}}^4)\]
where \(P_{\text{rad}}\) is the power radiated, \(\epsilon\) is the emissivity of the material, \(\sigma\) is the Stefan-Boltzmann constant, \(A\) is the area of the body, and \(T\) is the absolute temperature of the body's surface. Importantly, this relationship indicates an intense increase in radiated power with even a moderate rise in temperature, highlighting the significance of radiation in heat transfer scenarios at higher temperatures. For objects that are not perfect black bodies, which is most real-world cases, the emissivity factor adjusts the ratio to account for less than perfect radiation efficiency.
Radiation Heat Transfer
Radiation heat transfer is one of the three modes of heat transfer, the others being conduction and convection. What sets radiation apart is its ability to transfer energy through a vacuum—it does not require a medium. This type of heat transfer is based on electromagnetic waves and involves the emission of infrared radiation from heated objects.
In the context of our heater, radiation plays a pivotal role as the heater's temperature escalates. As the heater emits energy, some of that energy is absorbed, reflected, and transmitted by surrounding surfaces, ultimately altering the room's temperature distribution. Since heat radiation can occur without direct contact, it's crucial to consider the impact of surrounding surfaces' temperatures, such as the walls, especially when they're at different temperatures from the air.
Temperature-Heat Power Relationship
The temperature-heat power relationship is an essential concept in heat transfer, relating to how a change in power consumption affects an object's temperature. When all other factors remain constant, as power consumption increases, so does the temperature. This relationship, linear in cases without substantial radiation, becomes complex with increasing temperatures where radiation cannot be neglected.
In the electric heater scenario, the proportionality constant \(K\) represents the heater's efficiency at transferring heat to the surrounding air (assuming no radiation). When we neglect radiation, the relationship simplifies to (assuming \(K\) is constant):
\[P \propto (T - T_{\text{air}})\]
However, in real-life applications—and in our exercise—radiation's influence grows as temperatures increase, requiring the use of more nuanced calculations to accurately determine the heater's surface temperature at different power levels. This insight helps us grasp how the heater's efficiency can change with varying conditions.
Numerical Methods in Heat Transfer
Numerical methods in heat transfer are crucial for solving complicated problems that do not have straightforward analytical solutions. Such methods break down complex equations into more manageable calculations, often through iteration, to find approximate solutions.
To solve for the temperature of our electric heater when considering radiation, we turn to numerical methods because the relationship between power consumption, temperature, and radiated heat involves high-order polynomials due to the Stefan-Boltzmann Law. By implementing algorithms like the Newton-Raphson method or using computational software, we can iteratively hone in on the temperature value that balances the heat equation, accounting for both the direct heating (convection) and radiation effects.

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Most popular questions from this chapter

Four power transistors, each dissipating \(12 \mathrm{~W}\), are mounted on a thin vertical aluminum plate \(22 \mathrm{~cm} \times 22 \mathrm{~cm}\) in size. The heat generated by the transistors is to be dissipated by both surfaces of the plate to the surrounding air at \(25^{\circ} \mathrm{C}\), which is blown over the plate by a fan. The entire plate can be assumed to be nearly isothermal, and the exposed surface area of the transistor can be taken to be equal to its base area. If the average convection heat transfer coefficient is \(25 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), determine the temperature of the aluminum plate. Disregard any radiation effects.

The inner and outer surfaces of a 4-m \(\times 7-\mathrm{m}\) brick wall of thickness \(30 \mathrm{~cm}\) and thermal conductivity \(0.69 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\) are maintained at temperatures of \(26^{\circ} \mathrm{C}\) and \(8^{\circ} \mathrm{C}\), respectively. Determine the rate of heat transfer through the wall, in W.

Solar radiation is incident on a \(5 \mathrm{~m}^{2}\) solar absorber plate surface at a rate of \(800 \mathrm{~W} / \mathrm{m}^{2}\). Ninety-three percent of the solar radiation is absorbed by the absorber plate, while the remaining 7 percent is reflected away. The solar absorber plate has a surface temperature of \(40^{\circ} \mathrm{C}\) with an emissivity of \(0.9\) that experiences radiation exchange with the surrounding temperature of \(-5^{\circ} \mathrm{C}\). In addition, convective heat transfer occurs between the absorber plate surface and the ambient air of \(20^{\circ} \mathrm{C}\) with a convection heat transfer coefficient of \(7 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Determine the efficiency of the solar absorber, which is defined as the ratio of the usable heat collected by the absorber to the incident solar radiation on the absorber.

A solid plate, with a thickness of \(15 \mathrm{~cm}\) and a thermal conductivity of \(80 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\), is being cooled at the upper surface by air. The air temperature is \(10^{\circ} \mathrm{C}\), while the temperatures at the upper and lower surfaces of the plate are 50 and \(60^{\circ} \mathrm{C}\), respectively. Determine the convection heat transfer coefficient of air at the upper surface and discuss whether the value is reasonable or not for force convection of air.

How do \((a)\) draft and \((b)\) cold floor surfaces cause discomfort for a room's occupants?

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