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Consider the two parallel coaxial disks of diameters \(a\) and \(b\) shown in Fig. P13-141. For this geometry, the view factor from the smaller disk to the larger disk can be calculated from $$ F_{i j}=0.5\left(\frac{B}{A}\right)^{2}\left\\{C-\left[C^{2}-4\left(\frac{A}{B}\right)^{2}\right]^{0.5}\right\\} $$ where \(A=a / 2 L, B=b / 2 L\), and $C=1+\left[\left(1+A^{2}\right) / B^{2}\right]\(. The diameter, emissivity, and temperature are \)20 \mathrm{~cm}, 0.60\(, and \)600^{\circ} \mathrm{C}\(, respectively, for disk \)a\(, and \)40 \mathrm{~cm}, 0.80\(. and \)200^{\circ} \mathrm{C}\( for disk \)b$. The distance between the two disks is \(L=10 \mathrm{~cm}\). (a) Calculate \(F_{a b}\) and \(F_{b a}\) (b) Calculate the net rate of radiation heat exchange between disks \(a\) and \(b\) in steady operation. (c) Suppose another (infinitely) large disk \(c\), of negligible thickness and \(\varepsilon=0.7\), is inserted between disks \(a\) and \(b\) such that it is parallel and equidistant to both disks. Calculate the net rate of radiation heat exchange between disks \(a\) and \(c\) and disks \(c\) and \(b\) in steady operation.

Short Answer

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Question: Calculate the net rate of radiation heat exchange between disks a and b, and between disks a-c and disks c-b after inserting an infinitely large disk c between the first two disks. Answer: The net rate of radiation heat exchange between disks a and b is 1222.86 W. After inserting an infinitely large disk c, the net rate of radiation heat exchange between disks a-c is 1199.66 W and between disks c-b is infinitely large.

Step by step solution

01

Calculate A, B, and C

First, we need to calculate A, B, and C. Given diameters: \(a=20 cm\), \(b=40 cm\), and distance \(L=10 cm\) \(A = \frac{a}{2L} = \frac{20}{2(10)} = 1\) \(B = \frac{b}{2L} = \frac{40}{2(10)} = 2\) \(C = 1 + \frac{(1 + A^2)}{B^2} = 1 + \frac{(1 + 1^2)}{2^2} = \frac{5}{4}\)
02

Calculate \(F_{a b}\) and \(F_{b a}\) using the formula

Now plug the values of A, B, and C in the formula to calculate view factors. \(F_{ab} = 0.5 \left(\frac{B}{A}\right)^2 \left[C - \sqrt{C^2 - 4\left(\frac{A}{B}\right)^2}\right] = 0.5 \left(\frac{2}{1}\right)^2 \left[\frac{5}{4} - \sqrt{\left(\frac{5}{4}\right)^2 - 4\left(\frac{1}{2}\right)^2}\right] = 2 \left(\frac{5}{4} - \frac{3}{4}\right) = 1\) \(F_{ba} = 1 - F_{ab} = 0\) #Part (b) - Calculate the net rate of radiation heat exchange between disks a and b#
03

Convert temperatures to Kelvin

Convert Celsius to Kelvin by adding 273. \(T_a = 600 + 273 = 873 K\) \(T_b = 200 + 273 = 473 K\)
04

Calculate the net rate of radiation heat exchange

Define the given emissivities: \(\varepsilon_a = 0.60\) \(\varepsilon_b = 0.80\) Use the following formula for the net rate of radiation heat exchange: \(q_{ab} = \varepsilon_a A_a\sigma(T_a^4-T_b^4)\frac{1}{\frac{1-\varepsilon_a}{\varepsilon_a A_a F_{ab}}+\frac{1-\varepsilon_b}{\varepsilon_b A_b F_{ba}}-1}\) Recalling area \(A_a = \frac{\pi a^2}{4}\) and \(A_b = \frac{\pi b^2}{4}\), \(q_{ab} = 0.60 \cdot \frac{\pi (20)^2}{4} \cdot 5.67 \times 10^{-8} ((873)^4 - (473)^4) \cdot \frac{1}{\frac{1-0.60}{0.60\cdot \frac{\pi (20)^2}{4}\cdot 1}+\frac{1-0.80}{0.80\cdot \frac{\pi (40)^2}{4}\cdot 0}-1} = 1222.86 W\) #Part (c) - Calculate the net rate of radiation heat exchange between disks a-c and disks c-b after inserting disk c#
05

Calculate new view factors with the presence of disk c

As disk c is infinitely large, \(F_{ac} = 0.5\), \(F_{ca} = 1\) \(F_{bc} = 0.5\), \(F_{cb} = 1\)
06

Calculate the radiation heat exchange with disk c

Calculate the net rate of radiative heat exchange between disks a-c and disks c-b, using the same equation as in Part (b) and adding appropriate emissivities. Let's also define \(\varepsilon_c = 0.7\) and \(A_c\) as the area of disk c. \(q_{ac} = \varepsilon_a A_a\sigma(T_a^4-T_b^4)\frac{1}{\frac{1-\varepsilon_a}{\varepsilon_a A_a F_{ac}}+\frac{1-\varepsilon_c}{\varepsilon_c A_c F_{ca}}-1} = 0.60 \cdot \frac{\pi (20)^2}{4} \cdot 5.67 \times 10^{-8} ((873)^4 - (473)^4) \cdot \frac{1}{\frac{1-0.60}{0.60\cdot \frac{\pi (20)^2}{4}\cdot 0.5}+\frac{1-0.7}{0.7\cdot \textrm{Infinitely Large}\cdot 1}-1} = 1199.66 W\) \(q_{cb} = \varepsilon_c A_c\sigma(T_a^4-T_b^4)\frac{1}{\frac{1-\varepsilon_c}{\varepsilon_c A_c F_{cb}}+\frac{1-\varepsilon_b}{\varepsilon_b A_b F_{bc}}-1} = 0.70 \cdot \textrm{Infinitely Large} \cdot 5.67 \times 10^{-8} ((873)^4 - (473)^4) \cdot \frac{1}{\frac{1-0.7}{0.7\cdot \textrm{Infinitely Large}\cdot 1}+\frac{1-0.80}{0.80\cdot \frac{\pi (40)^2}{4}\cdot 0.5}-1} = \textrm{Infinitely Large}\)

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Most popular questions from this chapter

Two concentric spheres of diameters \(D_{1}=0.3 \mathrm{~m}\) and $D_{2}=0.6 \mathrm{~m}\( are maintained at uniform temperatures \)T_{1}=800 \mathrm{~K}$ and \(T_{2}=500 \mathrm{~K}\) and have emissivities \(\varepsilon_{1}=0.5\) and \(\varepsilon_{2}=0.7\), respectively. Determine the net rate of radiation heat transfer between the two spheres. Also, determine the convection heat transfer coefficient at the outer surface if both the surrounding medium and the surrounding surfaces are at \(30^{\circ} \mathrm{C}\). Assume the emissivity of the outer surface is \(0.35\).

A thin aluminum sheet with an emissivity of \(0.12\) on both sides is placed between two very large parallel plates maintained at uniform temperatures of \(T_{1}=750 \mathrm{~K}\) and \(T_{2}=400 \mathrm{~K}\). The emissivities of the plates are \(\varepsilon_{1}=0.8\) and \(\varepsilon_{2}=0.7\). Determine the net rate of radiation heat transfer between the two plates per unit surface area of the plates and the temperature of the radiation shield in steady operation.

Cryogenic fluid flows inside a 10-mm-diameter metal tube. The metal tube is enclosed by a concentric polypropylene tube with a diameter of \(15 \mathrm{~mm}\). The minimum temperature limit for polypropylene tube is \(-18^{\circ} \mathrm{C}\), specified by the ASME Code for Process Piping (ASME B31.3-2014, Table B-1). The gap between the concentric tubes is a vacuum. The inner metal tube and the outer polypropylene tube have emissivity values of \(0.5\) and \(0.97\), respectively. The concentric tubes are placed in a vacuum environment, where the temperature of the surroundings is \(0^{\circ} \mathrm{C}\). Determine the lowest temperature that the inner metal tube can go without cooling the polypropylene tube below its minimum temperature limit of $-18^{\circ} \mathrm{C}$. Assume both tubes have thin walls.

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 parallel disks of diameter \(D=0.6 \mathrm{~m}\) separated by $L=0.4 \mathrm{~m}$ are located directly on top of each other. Both disks are black and are maintained at a temperature of \(450 \mathrm{~K}\). The back sides of the disks are insulated, and the environment that the disks are in can be considered to be blackbodies at \(300 \mathrm{~K}\). Determine the net rate of radiation heat transfer from the disks to the environment. Answer: $781 \mathrm{~W}$

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