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 = 90 (2X+3) Where q0 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 70, respectively. Also, obtain temperature in the wall at X= 0.1 m. Assume, Ti-100 °C, T0-200 °C, L= 0.2 m, K = 40 w/m. °C, and q0 = 50 W 1 90 y FLUX

Principles of Heat Transfer (Activate Learning with these NEW titles from Engineering!)
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Author:Kreith, Frank; Manglik, Raj M.
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Chapter11: Heat Transfer By Radiation
Section: Chapter Questions
Problem 11.58P
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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 = 90 (2X+3)
Where q0 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 70, respectively. Also, obtain temperature in
the wall at X= 0.1 m. Assume, Ti-100 °C, T0-200 °C, L= 0.2 m, K = 40 w / m.
°C, and q0 = 50 W
To
X-
1 90
Y FLUX
Ti
Transcribed Image Text: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 = 90 (2X+3) Where q0 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 70, respectively. Also, obtain temperature in the wall at X= 0.1 m. Assume, Ti-100 °C, T0-200 °C, L= 0.2 m, K = 40 w / m. °C, and q0 = 50 W To X- 1 90 Y FLUX Ti
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