Chapter 13: Problem 107
Define the spectral transmissivity of a medium of thickness \(L\) in terms of \((a)\) spectral intensities and \((b)\) the spectral absorption coefficient.
Chapter 13: Problem 107
Define the spectral transmissivity of a medium of thickness \(L\) in terms of \((a)\) spectral intensities and \((b)\) the spectral absorption coefficient.
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Get started for freeA solar collector consists of a horizontal aluminum tube having an outer diameter of \(2.5\) in enclosed in a concentric thin glass tube of diameter $5 \mathrm{in}$. Water is heated as it flows through the tube, and the annular space between the aluminum and the glass tube is filled with air at $0.5 \mathrm{~atm}$ pressure. The pump circulating the water fails during a clear day, and the water temperature in the tube starts rising. The aluminum tube absorbs solar radiation at a rate of \(30 \mathrm{Btu} / \mathrm{h}\) per foot length, and the temperature of the ambient air outside is $75^{\circ} \mathrm{F}$. The emissivities of the tube and the glass cover are 0.9. Taking the effective sky temperature to be \(60^{\circ} \mathrm{F}\), determine the temperature of the aluminum tube when thermal equilibrium is established (i.e., when the rate of heat loss from the tube equals the amount of solar energy gained by the tube).
What is latent heat? How is the latent heat loss from the human body affected by \((a)\) skin wettedness and \((b)\) relative humidity of the environment? How is the rate of evaporation from the body related to the rate of latent heat loss?
A row of tubes, equally spaced at a distance that is twice the diameter of the tubes, is positioned between two large parallel plates. The surface temperature of the tubes is constant at \(10^{\circ} \mathrm{C}\) and the top and bottom plates are at constant temperatures of \(100^{\circ} \mathrm{C}\) and \(350^{\circ} \mathrm{C}\), respectively. If the surfaces behave as blackbody, determine the net radiation heat flux leaving the bottom plate.
Two thin radiation shields with emissivities of \(\varepsilon_{3}=0.10\) and \(\varepsilon_{4}=0.15\) on both sides are placed between two very large parallel plates, which are maintained at uniform temperatures $T_{1}=600 \mathrm{~K}\( and \)T_{2}=300 \mathrm{~K}$ and have emissivities \(\varepsilon_{1}=0.6\) and \(\varepsilon_{2}=0.7\), respectively (Fig. P13-103). Determine the net rates of radiation heat transfer between the two plates with and without the shields per unit surface area of the plates, and the temperatures of the radiation shields in steady operation.
Two very large parallel plates are maintained at uniform temperatures of \(T_{1}=1100 \mathrm{~K}\) and \(T_{2}=700 \mathrm{~K}\) and have emissivities of \(\varepsilon_{1}=\varepsilon_{2}=0.5\), respectively. It is desired to reduce the net rate of radiation heat transfer between the two plates to one-fifth by placing thin aluminum sheets with an emissivity of \(0.1\) on both sides between the plates. Determine the number of sheets that need to be inserted.
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