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While driving down a highway early in the evening, the airflow over an automobile establishes an overall heat transfer coefficient of $25 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$. The passenger cabin of this automobile exposes \(8 \mathrm{~m}^{2}\) of surface to the moving ambient air. On a day when the ambient temperature is \(33^{\circ} \mathrm{C}\), how much cooling must the air-conditioning system supply to maintain a temperature of $20^{\circ} \mathrm{C}$ in the passenger cabin? (a) \(0.65 \mathrm{MW}\) (b) \(1.4 \mathrm{MW}\) (c) \(2.6 \mathrm{MW}\) (d) \(3.5 \mathrm{MW}\) (e) \(0.94 \mathrm{MW}\)

Short Answer

Expert verified
Based on the given information and calculations, the cooling required by the air-conditioning system to maintain a temperature of \(20^{\circ} \mathrm{C}\) inside the passenger cabin is approximately \(2.6 \mathrm{kW}\) (or \(0.0026 \mathrm{MW}\), which is closest to option (c) \(2.6 \mathrm{MW}\)).

Step by step solution

01

Convert temperatures to Kelvin

First, we need to convert the given temperatures from Celsius to Kelvin. To do this, we need to add 273.15 to each temperature: \(T_a = 33^{\circ} \mathrm{C} + 273.15 = 306.15 \mathrm{K}\) \(T_c = 20^{\circ} \mathrm{C} + 273.15 = 293.15 \mathrm{K}\)
02

Calculate the cooling required (Q)

Now that we have the temperatures in Kelvin, we can use the heat transfer formula to calculate the cooling required by the air-conditioning system: \(Q = hA(T_a - T_c)\) Where \(h = 25 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), \(A = 8 \mathrm{~m}^{2}\), \(T_a = 306.15 \mathrm{K}\), and \(T_c = 293.15 \mathrm{K}\). \(Q = 25 \cdot 8(306.15 - 293.15)\)
03

Evaluate and find the answer

Now we can evaluate the expression to find the cooling required. \(Q = 25 \cdot 8 \cdot 13 = 2600 \mathrm{W} = 2.6 \mathrm{kW}\) From the given options, we see that \(2.6 \mathrm{kW}\) is closest to (c) \(2.6 \mathrm{MW}\), but we need to adjust the unit. Note that \(2.6 \mathrm{kW} = 0.0026 \mathrm{MW}\), which isn't one of the provided options. There might be a typographical error in the options, so we will go with the closest option which is (c) \(2.6 \mathrm{MW}\).

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Most popular questions from this chapter

Consider a person whose exposed surface area is \(1.7 \mathrm{~m}^{2}\), emissivity is \(0.5\), and surface temperature is \(32^{\circ} \mathrm{C}\). Determine the rate of heat loss from that person by radiation in a large room having walls at a temperature of (a) \(300 \mathrm{~K}\) and (b) $280 \mathrm{~K}$.

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.

A cylindrical fuel rod \(2 \mathrm{~cm}\) in diameter is encased in a concentric tube and cooled by water. The fuel generates heat uniformly at a rate of $150 \mathrm{MW} / \mathrm{m}^{3}$. The convection heat transfer coefficient on the fuel rod is \(5000 \mathrm{~W} / \mathrm{m}^{2}\). \(\mathrm{K}\), and the average temperature of the cooling water, sufficiently far from the fuel rod, is \(70^{\circ} \mathrm{C}\). Determine the surface temperature of the fuel rod, and discuss whether the value of the given convection heat transfer coefficient on the fuel rod is reasonable.

Consider steady heat transfer between two large parallel plates at constant temperatures of \(T_{1}=290 \mathrm{~K}\) and \(T_{2}=150 \mathrm{~K}\) that are \(L=2 \mathrm{~cm}\) apart. Assuming the surfaces to be black (emissivity \(\varepsilon=1\) ), determine the rate of heat transfer between the plates per unit surface area assuming the gap between the plates is \((a)\) filled with atmospheric air, \((b)\) evacuated, \((c)\) filled with fiberglass insulation, and \((d)\) filled with superinsulation having an apparent thermal conductivity of \(0.00015 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\).

A hollow spherical iron container with outer diameter \(20 \mathrm{~cm}\) and thickness \(0.2 \mathrm{~cm}\) is filled with iced water at $0^{\circ} \mathrm{C}\(. If the outer surface temperature is \)5^{\circ} \mathrm{C}$, determine the approximate rate of heat gain by the iced water in \(\mathrm{kW}\) and the rate at which ice melts in the container. The heat of fusion of water is \(333.7 \mathrm{~kJ} / \mathrm{kg}\). Treat the spherical shell as a plain wall, and use the outer area.

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