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The heat generated in the circuitry on the surface of a silicon chip $(k=130 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})$ is conducted to the ceramic substrate to which it is attached. The chip is $6 \mathrm{~mm} \times 6 \mathrm{~mm}\( in size and \)0.5 \mathrm{~mm}\( thick and dissipates \)3 \mathrm{~W}\( of power. Disregarding any heat transfer through the \)0.5$-mm- high side surfaces, determine the temperature difference between the front and back surfaces of the chip in steady operation.

Short Answer

Expert verified
Answer: The temperature difference between the front and back surfaces of the silicon chip is approximately 0.32 K.

Step by step solution

01

Convert given values into SI units

First, we need to make sure all dimensions are in SI units. The chip's thickness and dimensions should be expressed in meters, so we need to convert them from millimeters. The dimensions of the chip: - Length: 6 mm = 0.006 m - Width: 6 mm = 0.006 m - Thickness: 0.5 mm = 0.0005 m
02

Calculate the area through which heat is conducted

Next, compute the surface area of the chip: Area (A) = Length * Width = 0.006 m * 0.006 m = 0.000036 m^2
03

Use Fourier's law to find the temperature difference

Now use the Fourier's law of heat conduction: \(Q = k * A * \frac{\Delta T}{d}\) Rearrange the equation to solve for \(\Delta T\): \(\Delta T = \frac{Q * d}{k * A}\) Plug in the values: \(\Delta T = \frac{3 W * 0.0005 m}{130 W/m*K * 0.000036 m^2} = \frac{0.0015}{0.00468} = 0.320512\,\text{K}\)
04

Present the final result

Therefore, the temperature difference between the front and back surfaces of the silicon chip in steady operation is about 0.32 K.

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Most popular questions from this chapter

An engine block with a surface area measured to be \(0.95 \mathrm{~m}^{2}\) generates a power output of \(50 \mathrm{~kW}\) with a net engine efficiency of 35 percent. The engine block operates inside a compartment at $157^{\circ} \mathrm{C}\(, and the average convection heat transfer coefficient is \)50 \mathrm{~W} / \mathrm{m}^{2}\(. \)\mathrm{K}$. If convection is the only heat transfer mechanism occurring, determine the engine block surface temperature. Answer: \(841^{\circ} \mathrm{C}\)

Consider a sealed 20-cm-high electronic box whose base dimensions are $40 \mathrm{~cm} \times 40 \mathrm{~cm}$ placed in a vacuum chamber. The emissivity of the outer surface of the box is \(0.95\). If the electronic components in the box dissipate a total of \(100 \mathrm{~W}\) of power and the outer surface temperature of the box is not to exceed \(55^{\circ} \mathrm{C}\), determine the temperature at which the surrounding surfaces must be kept if this box is to be cooled by radiation alone. Assume the heat transfer from the bottom surface of the box to the stand to be negligible.

It is well known that wind makes the cold air feel much colder as a result of the wind-chill effect that is due to the increase in the convection heat transfer coefficient with increasing air velocity. The wind-chill effect is usually expressed in terms of the wind-chill temperature (WCT), which is the apparent temperature felt by exposed skin. For an outdoor air temperature of \(0^{\circ} \mathrm{C}\), for example, the windchill temperature is $-5^{\circ} \mathrm{C}\( with \)20 \mathrm{~km} / \mathrm{h}\( winds and \)-9^{\circ} \mathrm{C}\( with \)60 \mathrm{~km} / \mathrm{h}$ winds. That is, a person exposed to \(0^{\circ} \mathrm{C}\) windy air at \(20 \mathrm{~km} / \mathrm{h}\) will feel as cold as a person exposed to \(-5^{\circ} \mathrm{C}\) calm air (air motion under \(5 \mathrm{~km} / \mathrm{h}\) ). For heat transfer purposes, a standing man can be modeled as a 30 -cm- diameter, 170 -cm-long vertical cylinder with both the top and bottom surfaces insulated and with the side surface at an average temperature of $34^{\circ} \mathrm{C}\(. For a convection heat transfer coefficient of \)15 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$, determine the rate of heat loss from this man by convection in still air at \(20^{\circ} \mathrm{C}\). What would your answer be if the convection heat transfer coefficient is increased to $30 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$ as a result of winds? What is the wind-chill temperature in this case? Answers: $336 \mathrm{~W}, 672 \mathrm{~W}, 6^{\circ} \mathrm{C}$

Consider a 3-m \(\times 3-\mathrm{m} \times 3-\mathrm{m}\) cubical furnace whose top and side surfaces closely approximate black surfaces at a temperature of \(1200 \mathrm{~K}\). The base surface has an emissivity of \(\varepsilon=0.7\), and is maintained at \(800 \mathrm{~K}\). Determine the net rate of radiation heat transfer to the base surface from the top and side surfaces.

Water enters a pipe at \(20^{\circ} \mathrm{C}\) at a rate of $0.25 \mathrm{~kg} / \mathrm{s}\( and is heated to \)60^{\circ} \mathrm{C}$. The rate of heat transfer to the water is (a) \(10 \mathrm{~kW}\) (b) \(20.9 \mathrm{~kW}\) (c) \(41.8 \mathrm{~kW}\) (d) \(62.7 \mathrm{~kW}\) (e) \(167.2 \mathrm{~kW}\)

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