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A \(15-\mathrm{mm} \times 15-\mathrm{mm}\) silicon chip is mounted such that the edges are flush in a substrate. The chip dissipates \(1.4 \mathrm{~W}\) of power uniformly, while air at \(20^{\circ} \mathrm{C}\) ( $\left.1 \mathrm{~atm}\right)\( with a velocity of \)25 \mathrm{~m} / \mathrm{s}$ is used to cool the upper surface of the chip. If the substrate provides an unheated starting length of \(15 \mathrm{~mm}\), determine the surface temperature at the trailing edge of the chip. Evaluate the air properties at $50^{\circ} \mathrm{C}$.

Short Answer

Expert verified
Answer: The surface temperature at the trailing edge of the silicon chip is approximately \(49.15^{\circ} \mathrm{C}\).

Step by step solution

01

Calculate the heat flux and the convective heat transfer coefficient

Since we know the power dissipated by the chip, we can calculate the heat flux (q) by dividing the power dissipation (P) by the area of the silicon chip (A). \(q = \frac{P}{A}\) The area of the chip is: \(A = (15 \times 10^{-3} \text{m})\times(15 \times 10^{-3}\text{m})\) Plugging in the given values, we have: \(q = \frac{1.4\text{ W}}{(15 \times 10^{-3} \text{m})\times (15 \times 10^{-3}\text{m})} = 6256.25\,\text{W/m}^2\) Next, we need to calculate the convective heat transfer coefficient (h) by using the empirical correlation for forced convection over a flat plate, which is given by: \(h = (\text{St})\rho V C_p\) Where St is the Stanton Number, ρ is the air density, V is the air velocity, and C_p is the specific heat capacity of air at constant pressure. According to the empirical correlations, the Stanton Number (St) for a unit Reynolds number is approximately \(2.22 \times 10^{-5}\). The properties of the air at \(50^{\circ} \mathrm{C}\) are as follows: ρ = 1.164 \(\mathrm{kg/m^3}\), C_p = 1006.43 \(\mathrm{J/kg K}\). Now, we can calculate the convective heat transfer coefficient (h): \(h = (2.22 \times 10^{-5})\times(1.164 \,\mathrm{kg/m^3})\times (25 \,\mathrm{m/s})\times (1006.43 \,\mathrm{J/kgK}) = 684.54 \,\text{W/m}^2\text{K}\)
02

Determine surface temperature at the trailing edge

Now that we have the heat flux (q) and the convective heat transfer coefficient (h), we can find the surface temperature at the trailing edge of the chip. The temperature difference \((T_s - T_\infty)\) between the surface and the free-stream temperature can be found using the relation: \(q = h \times (T_s - T_\infty)\) Rearranging for \(T_s\) and using the given values, we have: \(T_s = \frac{q}{h} + T_\infty\) \(T_s = \frac{6256.25 \,\text{W/m}^2}{684.54 \,\text{W/m}^2\text{K}} + 20^{\circ} \mathrm{C} = 29.15^{\circ} \mathrm{C} + 20^{\circ} \mathrm{C} = 49.15^{\circ} \mathrm{C}\) Therefore, the surface temperature at the trailing edge of the chip is approximately \(49.15^{\circ} \mathrm{C}\).

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Most popular questions from this chapter

Air at \(20^{\circ} \mathrm{C}\) flows over a 4-m-long and 3-m-wide surface of a plate whose temperature is \(80^{\circ} \mathrm{C}\) with a velocity of $5 \mathrm{~m} / \mathrm{s}$. The rate of heat transfer from the laminar flow region of the surface is (a) \(950 \mathrm{~W}\) (b) \(1037 \mathrm{~W}\) (c) \(2074 \mathrm{~W}\) (d) \(2640 \mathrm{~W}\) (e) \(3075 \mathrm{~W}\) (For air, use $k=0.02735 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \operatorname{Pr}=0.7228, \nu=1.798 \times\( \)10^{-5} \mathrm{~m}^{2} / \mathrm{s}$ )

A thermocouple with a spherical junction diameter of \(1 \mathrm{~mm}\) is used for measuring the temperature of a hydrogen gas stream. The properties of the thermocouple junction are $k=35 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \rho=8500 \mathrm{~kg} / \mathrm{m}^{3}\(, and \)c_{p}=320 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}$. The hydrogen gas, behaving as an ideal gas at \(1 \mathrm{~atm}\), has a free-stream temperature of \(200^{\circ} \mathrm{C}\). If the initial temperature of the thermocouple junction is $10^{\circ} \mathrm{C}$, evaluate the time for the thermocouple to register 99 percent of the initial temperature difference at different free-stream velocities of the hydrogen gas. Using appropriate software, perform the evaluation by varying the free-stream velocity from 1 to \(100 \mathrm{~m} / \mathrm{s}\). Then, plot the thermocouple response time and the convection heat transfer coefficient as a function of free-stream velocity. Hint: Use the lumped system analysis to determine the time required for the thermocouple to register 99 percent of the initial temperature difference (verify the application of this method to this problem).

Repeat Prob. 7-137, assuming the inner surface of the tank to be at $0^{\circ} \mathrm{C}$ but by taking the thermal resistance of the tank and heat transfer by radiation into consideration. Assume the average surrounding surface temperature for radiation exchange to be \(25^{\circ} \mathrm{C}\) and the outer surface of the tank to have an emissivity of \(0.75\). Answers: (a) $379 \mathrm{~W}\(, (b) \)98.1 \mathrm{~kg}$

Air at \(15^{\circ} \mathrm{C}\) flows over a flat plate subjected to a uniform heat flux of \(240 \mathrm{~W} / \mathrm{m}^{2}\) with a velocity of $3.5 \mathrm{~m} / \mathrm{s}\(. The surface temperature of the plate \)6 \mathrm{~m}$ from the leading edge is (a) \(40.5^{\circ} \mathrm{C}\) (b) \(41.5^{\circ} \mathrm{C}\) (c) \(58.2^{\circ} \mathrm{C}\) (d) \(95.4^{\circ} \mathrm{C}\) (e) \(134^{\circ} \mathrm{C}\) (For air, use $k=0.02551 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \operatorname{Pr}=0.7296, \nu=1.562 \times\( \)10^{-5} \mathrm{~m}^{2} / \mathrm{s}$ )

A glass \((k=1.1 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) spherical tank is filled with chemicals undergoing exothermic reaction. The reaction keeps the inner surface temperature of the tank at \(80^{\circ} \mathrm{C}\). The tank has an inner radius of \(0.5 \mathrm{~m}\), and its wall thickness is $10 \mathrm{~mm}$. Situated in surroundings with an ambient temperature of \(15^{\circ} \mathrm{C}\) and a convection heat transfer coefficient of $70 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$, the tank's outer surface is being cooled by air flowing across it at \(5 \mathrm{~m} / \mathrm{s}\). In order to prevent thermal burn on individuals working around the container, it is necessary to keep the tank's outer surface temperature below $50^{\circ} \mathrm{C}$. Determine whether or not the tank's outer surface temperature is safe from thermal burn hazards.

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