Chapter 13: Problem 32
What are the two methods used in radiation analysis? How do these two methods differ?
Chapter 13: Problem 32
What are the two methods used in radiation analysis? How do these two methods differ?
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Get started for freeConsider 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) \(3084 \mathrm{~W}\)
Consider an infinitely long three-sided triangular enclosure with side lengths \(5 \mathrm{~cm}, 3 \mathrm{~cm}\), and \(4 \mathrm{~cm}\). The view factor from the \(5-\mathrm{cm}\) side to the \(4-\mathrm{cm}\) side is (a) \(0.3\) (b) \(0.4\) (c) \(0.5\) (d) \(0.6\) (e) \(0.7\)
Two very long concentric cylinders of diameters \(D_{1}=0.35 \mathrm{~m}\) and \(D_{2}=0.5 \mathrm{~m}\) are maintained at uniform temperatures of $T_{1}=950 \mathrm{~K}\( and \)T_{2}=500 \mathrm{~K}$ and have emissivities \(\varepsilon_{1}=1\) and \(\varepsilon_{2}=0.55\), respectively. Determine the net rate of radiation heat transfer between the two cylinders per unit length of the cylinders.
A 90 -cm-diameter flat black disk is placed in the center of the top surface of a \(1-m \times 1-m \times 1-m\) black box. The view factor from the entire interior surface of the box to the interior surface of the disk is (a) \(0.07\) (b) \(0.13\) (c) \(0.26\) (d) \(0.32\) (e) \(0.50\)
A flow-through combustion chamber consists of long, 15 -cm-diameter tubes immersed in water. Compressed air is routed to the tube, and fuel is sprayed into the compressed air. The combustion gases consist of 70 percent \(\mathrm{N}_{2}, 9\) percent \(\mathrm{H}_{2} \mathrm{O}, 15\) percent \(\mathrm{O}_{2}\), and 6 percent \(\mathrm{CO}_{2}\), and are maintained at $1 \mathrm{~atm}\( and \)1500 \mathrm{~K}$. The tube surfaces are near black, with an emissivity of \(0.9\). If the tubes are to be maintained at a temperature of \(600 \mathrm{~K}\), determine the rate of heat transfer from combustion gases to tube wall by radiation per \(m\) length of tube.
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