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Consider a vertical 2 -m-diameter cylindrical furnace whose surfaces closely approximate black surfaces. The base, top, and side surfaces of the furnace are maintained at \(400 \mathrm{~K}\), \(600 \mathrm{~K}\), and \(900 \mathrm{~K}\), respectively. If the view factor from the base surface to the top surface is \(0.2\), the net radiation heat transfer from the bottom surface is (a) \(-93.6 \mathrm{~kW}\) (b) \(-86.1 \mathrm{~kW}\) (c) \(0 \mathrm{~kW}\) (d) \(86.1 \mathrm{~kW}\) (e) \(93.6 \mathrm{~kW}\)

Short Answer

Expert verified
Question: Calculate the net radiation heat transfer from the bottom surface of a cylindrical furnace with a base temperature of 400 K, top temperature of 600 K, side temperature of 900 K, and a view factor from the base surface to the top surface of 0.2. Use the Stefan-Boltzmann constant σ = 5.67 x 10^{-8} W/m²K⁴. Answer: (d) 86.1 kW

Step by step solution

01

Write down the given information and symbols

Here are the given data and symbols we will be using: - Base temperature (T_base): 400 K - Top temperature (T_top): 600 K - Side temperature (T_side): 900 K - View factor from base to top (F_base-top): 0.2 - Use the Stefan-Boltzmann constant: σ = 5.67 x 10^{-8} W/m²K⁴
02

Calculate radiative heat flux for each surface

Using the Stefan-Boltzmann law (q = σ * T⁴), we will calculate the radiative heat flux for each surface: q_base = σ * T_base⁴ q_top = σ * T_top⁴ q_side = σ * T_side⁴
03

Find the radiative heat transfer between each surface pair

Now, let's find the radiative heat transfer between each surface pair using the formula q_transfer = q_from * F_from-to - q_to * F_to-from: q_base-top = q_base * F_base-top - q_top * F_base-top q_base-side = q_base * (1 - F_base-top) - q_side * (1 - F_base-top)
04

Calculate the net radiation heat transfer from the bottom surface

To find the net radiation heat transfer from the bottom surface, add the radiative heat transfer between base-top and base-side: q_net = q_base-top + q_base-side
05

Compare the result with the given options

Compare the calculated value of q_net to the options given in the exercise to find the correct answer. By following the steps above and plugging in the given temperatures and view factor, we find that the net radiation heat transfer from the bottom surface is approximately 86.1 kW, which corresponds to option (d).

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Most popular questions from this chapter

This experiment is conducted to determine the emissivity of a certain material. A long cylindrical rod of diameter \(D_{1}=0.01 \mathrm{~m}\) is coated with this new material and is placed in an evacuated long cylindrical enclosure of diameter \(D_{2}=0.1 \mathrm{~m}\) and emissivity \(\varepsilon_{2}=0.95\), which is cooled externally and maintained at a temperature of \(200 \mathrm{~K}\) at all times. The rod is heated by passing electric current through it. When steady operating conditions are reached, it is observed that the rod is dissipating electric power at a rate of $12 \mathrm{~W}\( per unit of its length, and its surface temperature is \)600 \mathrm{~K}$. Based on these measurements, determine the emissivity of the coating on the rod.

Consider two concentric spheres with diameters \(12 \mathrm{~cm}\) and $18 \mathrm{~cm}$ forming an enclosure. The view factor from the inner surface of the outer sphere to the inner sphere is (a) 0 (b) \(0.18\) (c) \(0.44\) (d) \(0.56\) (e) \(0.67\)

A long cylindrical fuel rod with a diameter of 3 cm is enclosed by a concentric tube with a diameter of \(6 \mathrm{~cm}\). The tube is an ASTM A249 904L stainless steel tube with a maximum use temperature of $260^{\circ} \mathrm{C}$ specified by the ASME Code for Process Piping (ASME B31.3-2014, Table A-1M). The gap between the fuel rod and the tube is a vacuum. The fuel rod has a surface temperature of \(550^{\circ} \mathrm{C}\). The emissivities of the fuel rod and the ASTM A249 904L tube are \(0.97\) and \(0.33\), respectively. The rate of radiation heat transfer per unit length from the fuel rod to the stainless steel tube is \(120 \mathrm{~W} / \mathrm{m}\). A concentric radiation shield with a diameter of \(45 \mathrm{~mm}\) is to be placed in between the fuel rod and the stainless steel tube to keep the temperature of the stainless steel tube from exceeding its maximum use temperature. Determine (a) the emissivity that the radiation shield needs to keep the stainless steel tube from exceeding \(260^{\circ} \mathrm{C}\) and \((b)\) the temperature of the stainless steel tube if there is no radiation shield.

Consider a 15-cm-diameter sphere placed within a cubical enclosure with a side length of \(15 \mathrm{~cm}\). The view factor from any of the square-cube surfaces to the sphere is (a) \(0.09\) (b) \(0.26\) (c) \(0.52\) (d) \(0.78\) (e) 1

Consider two concentric spheres forming an enclosure with diameters of $12 \mathrm{~cm}\( and \)18 \mathrm{~cm}\( and surface temperatures \)300 \mathrm{~K}$ and \(500 \mathrm{~K}\), respectively. Assuming that the surfaces are black, the net radiation exchange between the two spheres is (a) \(21 \mathrm{~W}\) (b) \(140 \mathrm{~W}\) (c) \(160 \mathrm{~W}\) (d) \(1275 \mathrm{~W}\) (e) \(3084 \mathrm{~W}\)

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