take into consideration one-dimensional conduction in a aircraft composite wall. The outer surfaces room exposed to a fluid at 25°C and a convection warmth transfer coefficient of 1000 W/m2 ∙ K. The middle wall B experience uniform heat generation B, while there is no generation in walls A and C. The temperatures at the interfaces room T1 = 261°C and T2 = 211°C.

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(a) presume negligible call resistance in ~ the interfaces, determine the volumetric heat generation B and also the thermal conductivity kB.

(b) Plot the temperature distribution, mirroring its crucial features.

(c) Consider conditions corresponding come a ns of coolant at the exposed surface of material A (h = 0). Identify T1 and T2 and plot the temperature circulation throughout the system.

 


jan 27 2021 06:23 am

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VENKATA S answer on January 29, 2021

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