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A horizontal \(1.5\)-m-wide, \(4.5\)-m-long double-pane window consists of two sheets of glass separated by a \(3.5-\mathrm{cm}\) gap filled with water. If the glass surface temperatures at the bottom and the top are measured to be \(60^{\circ} \mathrm{C}\) and \(40^{\circ} \mathrm{C}\), respectively, the rate of heat transfer through the window is (a) \(27.6 \mathrm{~kW}\) (b) \(39.4 \mathrm{~kW}\) (c) \(59.6 \mathrm{~kW}\) (d) \(66.4 \mathrm{~kW}\) (e) \(75.5 \mathrm{~kW}\) (For water, use $k=0.644 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \quad \operatorname{Pr}=3.55\(, \)\nu=0.554 \times 10^{-6} \mathrm{~m}^{2} / \mathrm{s}, \beta=0.451 \times 10^{-3} \mathrm{~K}^{-1}$. Also, the applicable correlation is \(\mathrm{Nu}=0.069 \mathrm{Ra}^{1 / 3} \mathrm{Pr}^{0.074}\).)

Short Answer

Expert verified
Answer: To find the rate of heat transfer, follow the steps of calculating the temperature difference, Rayleigh number, Nusselt number, heat transfer coefficient, and heat transfer rate. Once you have calculated the heat transfer rate (Q), compare it with the given options to find the correct answer.

Step by step solution

01

Calculating temperature difference

First, calculate the temperature difference between the bottom and top of the window (\(ΔT\)): \(ΔT = 60^{\circ}\mathrm{C} - 40^{\circ}\mathrm{C} = 20^{\circ}\mathrm{C} \)
02

Calculating the Rayleigh number

Calculate the Rayleigh number (Ra) using the formula: \(Ra = \frac{g\beta ΔTL^{3}}{να}\) First, we need to find α. α is the thermal diffusivity which equals to: \(α = \frac{k}{ρc_p}\) We know that for water, \(k = 0.644 \frac{\mathrm{W}}{\mathrm{m}⋅\mathrm{K}}\), \(ν = 0.554×10^{-6} \frac{\mathrm{m}^{2}}{\mathrm{s}}\), and \(\beta = 0.451×10^{-3} K^{-1}\). Also, Prandtl number (\(Pr\)) \(= 3.55\). We will start by finding α using Prandtl number: \(Pr = \frac{ν}{α}\) => \(α = \frac{ν}{Pr} = \frac{0.554×10^{-6}\frac{\mathrm{m}^2}{\mathrm{s}}}{3.55}\) Now we can calculate Ra: \(Ra = \frac{9.81 \times 0.451×10^{-3} K^{-1} \times 20 K \times(3.5×10^{-2} m)^3}{0.554×10^{-6} \frac{\mathrm{m}^{2}}{\mathrm{s}} \times \frac{0.554×10^{-6}\frac{\mathrm{m}^2}{\mathrm{s}}}{3.55}}\)
03

Calculating the Nusselt number

Calculate the Nusselt number (Nu) using the given correlation: \(Nu = 0.069 \times Ra^{1/3} \times Pr^{0.074}\) By inserting the previously calculated values, we get: \(Nu = 0.069 \times Ra^{1/3} \times 3.55^{0.074}\)
04

Calculating heat transfer coefficient

Find the heat transfer coefficient (\(h\)) using Nusselt number: \(h = \frac{Nu \times k}{L}\) Inserting the calculated Nusselt number: \(h = \frac{Nu \times 0.644 \frac{\mathrm{W}}{\mathrm{m}⋅\mathrm{K}}}{3.5×10^{-2} m}\)
05

Calculating heat transfer rate

Finally, we calculate the heat transfer rate (\(Q\)) using the formula: \(Q = h \times A \times ΔT\) where \(A\) is the area of the window, and it is given by: \(A = 1.5\,\mathrm{m} \times 4.5\,\mathrm{m}\) By inserting the relevant values, we get: \(Q = h \times (1.5\,\mathrm{m} \times 4.5\,\mathrm{m}) \times 20\,K\) Now, compare the calculated value of Q with the given options to find the correct answer.

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Most popular questions from this chapter

Consider a heat sink with optimum fin spacing. Explain how heat transfer from this heat sink will be affected by \((a)\) removing some of the fins on the heat sink and (b) doubling the number of fins on the heat sink by reducing the fin spacing. The base area of the heat sink remains unchanged at all times.

A hot liquid $\left(c_{p}=1000 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\( flows at a flow rate of \)0.05 \mathrm{~kg} / \mathrm{s}$ inside a copper pipe with an inner diameter of \(45 \mathrm{~mm}\) and a wall thickness of \(5 \mathrm{~mm}\). At the pipe exit, the liquid temperature decreases by \(10^{\circ} \mathrm{C}\) from its temperature at the inlet. The outer surface of the \(5-\mathrm{m}\)-long copper pipe is black oxidized, which subjects the outer surface to radiation heat transfer. The air temperature surrounding the pipe is \(10^{\circ} \mathrm{C}\). Assuming that the properties of air can be evaluated at \(35^{\circ} \mathrm{C}\) and \(1 \mathrm{~atm}\) pressure, determine the outer surface temperature of the pipe. Is $35^{\circ} \mathrm{C}$ an appropriate film temperature for evaluation of the air properties?

Hot engine oil is being transported in a horizontal pipe $\left(k=15 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, D_{i}=5 \mathrm{~cm}\right)$ with a wall thickness of \(5 \mathrm{~mm}\). The pipe is covered with a \(5-\mathrm{mm}\)-thick layer of insulation $(k=0.15 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\(. A length of \)2 \mathrm{~m}$ of the outer surface is exposed to cool air at \(10^{\circ} \mathrm{C}\). If the pipe inner surface temperature is at \(90^{\circ} \mathrm{C}\), determine the outer surface temperature. Hint: The pipe outer surface temperature has to be found iteratively. Begin the calculations by using a film temperature of $50^{\circ} \mathrm{C}$.

A boiler supplies hot water to equipment through a horizontal pipe. The hot water exits the pipe and enters the equipment at \(98^{\circ} \mathrm{C}\). The outer diameter of the pipe is \(20 \mathrm{~mm}\), and the pipe distance between the boiler and the equipment is \(30 \mathrm{~m}\). The section of the pipe between the boiler and the equipment is exposed to natural convection with air at an ambient temperature of \(20^{\circ} \mathrm{C}\). The hot water flows steadily in the pipe at \(10 \mathrm{~g} / \mathrm{s}\), and its specific heat is \(4.2 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\). The temperature at the pipe surface is \(80^{\circ} \mathrm{C}\), and the pipe has an emissivity of \(0.6\) that contributes to the thermal radiation with the surroundings at \(20^{\circ} \mathrm{C}\). According to the service restrictions of the ASME Boiler and Pressure Vessel Code (ASME BPVC.IV-2015, HG-101), hot water boilers should not be operating at temperatures exceeding \(120^{\circ} \mathrm{C}\) at or near the boiler outlet. Determine whether the water temperature exiting the boiler is in compliance with the ASME Boiler and Pressure Vessel Code.

A \(0.5-\mathrm{m}\)-long thin vertical copper plate is subjected to a uniform heat flux of \(1000 \mathrm{~W} / \mathrm{m}^{2}\) on one side, while the other side is exposed to air at \(5^{\circ} \mathrm{C}\). Determine the plate midpoint temperature for \((a)\) a highly polished surface and \((b)\) a black oxidized surface. Hint: The plate midpoint temperature \(\left(T_{L 2}\right)\) has to be found iteratively. Begin the calculations by using a film temperature of \(30^{\circ} \mathrm{C}\).

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