composite wall of combustion chamber contains material UI and material II. The A temperatures at the both end faces of the chamber are 200 K and 100 K The thermal conductivity (k) and thickness (t) of materials I and I are as follows 1 0.20 m W 0,015 mK 1I 0.10 m W 0.02 m K Calculate the heat flux and the temperature between the materials I and II
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