The surface of a radiation shield facing a black hot wall at 400 K has a reflectivity of 0.95. Attached to the back side of the shield is a 25-mm-thick sheet of insulating material having a thermal conductivity of 0.016 W/m ⋅ K . The overall heat transfer coefficient (convection and radiation) at the surface exposed to the ambient air and surroundings al 300 K is 10 W/m 2 ⋅ K . (a) Assuming negligible convection in the region between the wall and the shield, estimate the heat loss per unit area from the hot wall. (b) Perform a parameter sensitivity analysis on the insulation system, considering the effects of shield reflectivity, ρ s , and insulation thermal conductivity, k . What influence do these parameters have on the heat loss from the hot wall? What is the effect of an increased overall coefficient on the heal loss? Show the results of your analysis in a graphical format.
The surface of a radiation shield facing a black hot wall at 400 K has a reflectivity of 0.95. Attached to the back side of the shield is a 25-mm-thick sheet of insulating material having a thermal conductivity of 0.016 W/m ⋅ K . The overall heat transfer coefficient (convection and radiation) at the surface exposed to the ambient air and surroundings al 300 K is 10 W/m 2 ⋅ K . (a) Assuming negligible convection in the region between the wall and the shield, estimate the heat loss per unit area from the hot wall. (b) Perform a parameter sensitivity analysis on the insulation system, considering the effects of shield reflectivity, ρ s , and insulation thermal conductivity, k . What influence do these parameters have on the heat loss from the hot wall? What is the effect of an increased overall coefficient on the heal loss? Show the results of your analysis in a graphical format.
Solution Summary: The author explains how to perform the energy balance on shield and the wall.
The surface of a radiation shield facing a black hot wall at 400 K has a reflectivity of 0.95. Attached to the back side of the shield is a 25-mm-thick sheet of insulating material having a thermal conductivity of
0.016
W/m
⋅
K
. The overall heat transfer coefficient (convection and radiation) at the surface exposed to the ambient air and surroundings al 300 K is
10
W/m
2
⋅
K
.
(a) Assuming negligible convection in the region between the wall and the shield, estimate the heat loss per unit area from the hot wall. (b) Perform a parameter sensitivity analysis on the insulation system, considering the effects of shield reflectivity,
ρ
s
, and insulation thermal conductivity, k. What influence do these parameters have on the heat loss from the hot wall? What is the effect of an increased overall coefficient on the heal loss? Show the results of your analysis in a graphical format.
A plate-type solar energy collectorr with an absorbing surface covered by a glass is to receive an incident radiation of 800 W/m2. The glass plate has a reflectivity of 0.12 and a transmissivity of 0.80. The absorbing surface has an absorptivity of 0.90. The area of the collector is 5 m2. How much solar energy in watts is absorbed by the collector?
ANSWER: 3060 WATTS
Two plates are separated by two radiation shields with emissivities of 0.10 and 0.15for both sides. The two plates are said to have maintained uniform temperatures600 K (emissivity = 0.6) and 300 K (emissivity = 0.7). Calculate the net rate of heattransfer (W/m2) between the two plates with and without the shields per unitsurface area. Determine the rate of heat transfer (W/m2) between the two plateswhen one plate (emissivity = 0.10) is removed. Assume that the temperatures ofradiations shield are in steady operation.
Two long parallel plates of same emissivity 0.5 are
maintained at different temperatures and have radiation
heat exchange between them. The radiation shield of
emissivity 0.25 placed in the middle will reduce radiation
heat exchange to
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