For one -dimension heat transfer conduction consider a shielding wall for a nuclear reactor. The wall receives a gamma-ray flux such that heat is generated within the wall according to the relation = 9, ( 2X+3) Where g0 is the heat generation at the inner face of the wall exposed to the gamma- ray Flux. Using this relation for heat generation, derive an expression for the temperature distribution in a wall of thickness L, where the inside and outside temperatures are maintained at Ti and TO, respectively. Also, obtain temperature in the wall at X= 0.1 m. Assume, Ti-100 °C, TO=200 °C, L= 0.2 m, K = 40 w / m. °C, and q0 = 50 W 1 90 y FLUX То Ti

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Chapter2: Steady Heat Conduction
Section: Chapter Questions
Problem 2.29P: 2.29 In a cylindrical fuel rod of a nuclear reactor, heat is generated internally according to the...
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Q1
For one -dimension heat transfer conduction consider a shielding wall for a nuclear
reactor. The wall receives a gamma-ray flux such that heat is generated within the
wall according to the relation
9x = 4, ( 2X+3)
Where q0 is the heat generation at the inner face of the wall exposed to the
ray Flux. Using this relation for heat generation, derive an expression for the
temperature distribution in a wall of thickness L, where the inside and outside
temperatures are maintained at Ti and TO, respectively. Also, obtain temperature in
the wall at X= 0.1 m. Assume, Ti-100 °C, TO=200 °C, L= 0.2 m, K = 40 w/ m.
°C, and q0 = 50 W
%D
gamma-
%3D
I 90
y FLUX
То
Ti
Transcribed Image Text:Q1 For one -dimension heat transfer conduction consider a shielding wall for a nuclear reactor. The wall receives a gamma-ray flux such that heat is generated within the wall according to the relation 9x = 4, ( 2X+3) Where q0 is the heat generation at the inner face of the wall exposed to the ray Flux. Using this relation for heat generation, derive an expression for the temperature distribution in a wall of thickness L, where the inside and outside temperatures are maintained at Ti and TO, respectively. Also, obtain temperature in the wall at X= 0.1 m. Assume, Ti-100 °C, TO=200 °C, L= 0.2 m, K = 40 w/ m. °C, and q0 = 50 W %D gamma- %3D I 90 y FLUX То Ti
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