22. Develop an algorithm, along with the program (preferably in python), to find the temperature distribution in the example below NOTE: Use the explicit finite differences method EXAMPLE 5.9 A fuel element of a nuclear reactor is in the shape of a plane wall of thickness 2L = 20 mm and is convectively cooled at both surfaces, with h = 1100 W/m². K and T=250°C. At normal operating power, heat is generated uniformly within the element at a volumetric rate of q₁ = 107 W/m³. A departure from the steady-state conditions associated with normal operation will occur if there is a change in the generation rate. Consider a sudden change to q₂ = 2 × 107 W/m³, and use the explicit finite-difference method to determine the fuel element temperature distribu- tion after 1.5 s. The fuel element thermal properties are k = 30 W/m . K and a = 5 × 10-6 m²/s.

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Chapter8: Natural Convection
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Problem 8.27P
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22. Develop an algorithm, along with the program (preferably in python), to find the
temperature distribution in the example below
NOTE: Use the explicit finite differences method
EXAMPLE 5.9
A fuel element of a nuclear reactor is in the shape of a plane wall of thickness
2L = 20 mm and is convectively cooled at both surfaces, with h = 1100 W/m². K
and T=250°C. At normal operating power, heat is generated uniformly within the
element at a volumetric rate of q₁ = 107 W/m³. A departure from the steady-state
conditions associated with normal operation will occur if there is a change in the
generation rate. Consider a sudden change to q₂ = 2 × 107 W/m³, and use the
explicit finite-difference method to determine the fuel element temperature distribu-
tion after 1.5 s. The fuel element thermal properties are k = 30 W/m . K and a =
5 × 10-6 m²/s.
Transcribed Image Text:22. Develop an algorithm, along with the program (preferably in python), to find the temperature distribution in the example below NOTE: Use the explicit finite differences method EXAMPLE 5.9 A fuel element of a nuclear reactor is in the shape of a plane wall of thickness 2L = 20 mm and is convectively cooled at both surfaces, with h = 1100 W/m². K and T=250°C. At normal operating power, heat is generated uniformly within the element at a volumetric rate of q₁ = 107 W/m³. A departure from the steady-state conditions associated with normal operation will occur if there is a change in the generation rate. Consider a sudden change to q₂ = 2 × 107 W/m³, and use the explicit finite-difference method to determine the fuel element temperature distribu- tion after 1.5 s. The fuel element thermal properties are k = 30 W/m . K and a = 5 × 10-6 m²/s.
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