Radiation Shield Wall

Find the heat transfer per unit area due to radiation between two infinite long parallel planes. The first plane has emissivity 0.4 and is maintained at 245oC. The emissivity of the second plane is 0.2 and maintained at 27oC. A radiation shield having emissivity of 0.5 is introduced between given two planes. Find the percentage reduction in the heat transfer rate. Refer the image in simulation.
PercentageReduction=(QA)w(QA)s(QA)w100 Percentage Reduction = \frac{(\frac{Q}{A})_w - (\frac{Q}{A})_s}{(\frac{Q}{A})_w} * 100
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Find the heat transfer per unit area due to radiation between two infinite long parallel planes. The first plane has emissivity 0.4 and is maintained at 245oC. The emissivity of the second plane is 0.2 and maintained at 27oC. A radiation shield having emissivity of 0.5 is introduced between given two planes. Find the steady state temperature of the shield. Refer the image in simulation.
T3=[QAs1ϵ1+1ϵ31σT14] T_3 = [\frac{- \frac{Q}{A}_s \frac{1}{\epsilon_1}+\frac{1}{\epsilon_3} - 1}{\sigma}{T_1^4}]
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