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Two concentric spheres are maintained at uniform temperatures \(T_{1}=45^{\circ} \mathrm{C}\) and \(T_{2}=280^{\circ} \mathrm{C}\) and have emissivities \(\varepsilon_{1}=0.25\) and \(\varepsilon_{2}=0.7\), respectively. If the ratio of the diameters is \(D_{1} / D_{2}=0.30\), the net rate of radiation heat transfer between the two spheres per unit surface area of the inner sphere is (a) \(86 \mathrm{~W} / \mathrm{m}^{2}\) (b) \(1169 \mathrm{~W} / \mathrm{m}^{2}\) (c) \(1181 \mathrm{~W} / \mathrm{m}^{2}\) (d) \(2510 \mathrm{~W} / \mathrm{m}^{2}\) (e) \(3306 \mathrm{~W} / \mathrm{m}^{2}\)

Short Answer

Expert verified
Answer: (c) 1181 W/m²

Step by step solution

01

Convert temperatures to Kelvin

Given temperatures are \(T_1=45^\circ \mathrm{C}\) and \(T_2=280^\circ \mathrm{C}\). To convert them to Kelvin, we need to add 273 to both values: $$T_{1K} = T_1 + 273 = 45 + 273 = 318\, \mathrm{K}$$ $$T_{2K} = T_2 + 273 = 280 + 273 = 553\, \mathrm{K}$$
02

Calculate the surface areas

Given the ratio of the diameters \(D_1 / D_2 = 0.30\). Since the surface area of a sphere with diameter \(D\) is \(A = \pi D^2\), we can substitute the relation of diameters to the surface areas: $$\frac{A_1}{A_2} = \left(\frac{D_1}{D_2}\right)^2 = 0.30^2 = 0.09$$ Let \(A_2 = k\), then \(A_1 = 0.09 k\). Here, \(k\) is just an arbitrary parameter representing the actual surface area of sphere 2.
03

Apply the formula

Now, let's plug the given values into the formula for the net rate of radiation heat transfer: $$ H_{net} = \frac{\varepsilon_1 \sigma T_1^4 - \varepsilon_2 \sigma T_2^4}{\frac{1 - \varepsilon_1}{\varepsilon_1 A_1} + \frac{1 - \varepsilon_2}{\varepsilon_2 A_2}} = \frac{0.25 \sigma (318)^4 - 0.7\sigma (553)^4}{\frac{1 - 0.25}{0.25 (0.09k)} + \frac{1 - 0.7}{0.7 k}} $$
04

Simplify and find the answer

Let's simplify the equation to find the value of \(H_{net}\): $$ H_{net} = \frac{0.25\sigma (318)^4 - 0.7\sigma (553)^4}{\frac{0.75}{0.0225k} + \frac{0.3}{0.7 k}} = \frac{0.25\sigma (318)^4 - 0.7\sigma (553)^4}{\frac{1}{k}}k = 0.25\sigma (318)^4 - 0.7\sigma (553)^4 $$ Now, evaluate the value of H_net using \(\sigma = 5.67 \times 10^{-8} Wm^{-2}K^{-4}\): $$ H_{net} = 0.25(5.67 \times 10^{-8})(318)^4 - 0.7(5.67 \times 10^{-8})(553)^4 \approx 1181 \, \mathrm{W/m^2} $$ Hence, the correct option is (c) \(1181 \, \mathrm{W/m^2}\).

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Most popular questions from this chapter

Consider a long semicylindrical duct of diameter \(1.0 \mathrm{~m}\). Heat is supplied from the base surface, which is black, at a rate of $1200 \mathrm{~W} / \mathrm{m}^{2}\(, while the side surface with an emissivity of \)0.4$ is maintained at \(650 \mathrm{~K}\). Neglecting the end effects, determine the temperature of the base surface.

Explain all the different mechanisms of heat transfer from the human body \((a)\) through the skin and \((b)\) through the lungs.

A dryer is shaped like a long semicylindrical duct of diameter $1.5 \mathrm{~m}$. The base of the dryer is occupied by watersoaked materials to be dried, and it is maintained at a temperature of \(370 \mathrm{~K}\) and emissivity of \(0.5\). The dome of the dryer is maintained at \(1000 \mathrm{~K}\) with emissivity of \(0.8\). Determine the drying rate per unit length experienced by the wet materials.

Two square plates, with the sides \(a\) and \(b\) (and \(b>a\) ), are coaxial and parallel to each other, as shown in Fig. P13-142, and they are separated by a center-to-center distance of \(L\). The radiation view factor from the smaller to the larger plate, \(F_{a b+}\) is given by $$ F_{a b}=\frac{1}{2 A}\left\\{\left[(B+A)^{2}+4\right]^{0.5}-\left[(B-A)^{2}+4\right]^{0.5}\right\\} $$ where, \(A=a / L\) and \(B=b / L\). (a) Calculate the view factors \(F_{a b}\) and \(F_{b a}\) for $a=20 \mathrm{~cm}\(, \)b=60 \mathrm{~cm}\(, and \)L=40 \mathrm{~cm}$. (b) Calculate the net rate of radiation heat exchange between the two plates described above if \(T_{a}=800^{\circ} \mathrm{C}\), $T_{b}=200^{\circ} \mathrm{C}, \varepsilon_{a}=0.8\(, and \)\varepsilon_{b}=0.4$. (c) A large, square plate (with the side $c=2.0 \mathrm{~m}, \varepsilon_{c}=0.1$, and negligible thickness) is inserted symmetrically between the two plates such that it is parallel to and equidistant from them. For the data given above, calculate the temperature of this third plate when steady operating conditions are established.

Air is flowing between two infinitely large parallel plates. The upper plate is at \(500 \mathrm{~K}\) and has an emissivity of \(0.7\), while the lower plate is a black surface with temperature at \(330 \mathrm{~K}\). If the air temperature is \(290 \mathrm{~K}\), determine the convection heat transfer coefficient associated with the air.

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