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Calculated thermal conductance for radia...

Calculated thermal conductance for radial flow of a spherical sheel of inner and outer radius `r_(1)`and `r_(2)`. Assume that thermal conductivity of the material is `K`

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To calculate the thermal conductance \( G \) for the radial flow of a spherical shell with inner radius \( r_1 \) and outer radius \( r_2 \), and given thermal conductivity \( K \), we can follow these steps: ### Step 1: Understand the Concept of Thermal Resistance The thermal resistance \( R \) for a spherical shell can be expressed as: \[ R = \frac{L}{KA} \] where: - \( L \) is the thickness of the shell, - \( K \) is the thermal conductivity, - \( A \) is the surface area. ### Step 2: Define the Variables For a spherical shell, the thickness \( dR \) is an infinitesimal change in radius, and the surface area \( A \) at a radius \( r \) is given by: \[ A = 4\pi r^2 \] ### Step 3: Express the Thermal Resistance The thermal resistance \( dR \) for an infinitesimal thickness \( dR \) can be expressed as: \[ dR = \frac{dR}{K \cdot 4\pi r^2} \] ### Step 4: Integrate the Thermal Resistance To find the total thermal resistance from \( r_1 \) to \( r_2 \), we integrate: \[ R = \int_{r_1}^{r_2} \frac{dR}{K \cdot 4\pi r^2} \] This simplifies to: \[ R = \frac{1}{K \cdot 4\pi} \int_{r_1}^{r_2} \frac{1}{r^2} dR \] ### Step 5: Solve the Integral The integral of \( \frac{1}{r^2} \) is: \[ \int \frac{1}{r^2} dR = -\frac{1}{r} \] Thus, we have: \[ R = \frac{1}{K \cdot 4\pi} \left[-\frac{1}{r}\right]_{r_1}^{r_2} \] Evaluating the limits gives: \[ R = \frac{1}{K \cdot 4\pi} \left(-\frac{1}{r_2} + \frac{1}{r_1}\right) = \frac{1}{K \cdot 4\pi} \left(\frac{1}{r_1} - \frac{1}{r_2}\right) \] ### Step 6: Calculate the Thermal Conductance The thermal conductance \( G \) is the reciprocal of the thermal resistance \( R \): \[ G = \frac{1}{R} = \frac{K \cdot 4\pi}{\frac{1}{r_1} - \frac{1}{r_2}} \] This can be simplified further: \[ G = \frac{4\pi K r_1 r_2}{r_2 - r_1} \] ### Final Result Thus, the thermal conductance for the radial flow of a spherical shell is: \[ G = \frac{4\pi K r_1 r_2}{r_2 - r_1} \]

To calculate the thermal conductance \( G \) for the radial flow of a spherical shell with inner radius \( r_1 \) and outer radius \( r_2 \), and given thermal conductivity \( K \), we can follow these steps: ### Step 1: Understand the Concept of Thermal Resistance The thermal resistance \( R \) for a spherical shell can be expressed as: \[ R = \frac{L}{KA} \] where: ...
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