Step 1: Understanding Heat Transfer Through Composite Slabs
The heat transfer rate \( Q \) through a composite slab in steady-state condition is the same through both materials: \[ \frac{K_1 A (T_1 - T)}{d} = \frac{K_2 A (T - T_2)}{d}. \] where: - \( K_1, K_2 \) are the thermal conductivities of copper and brass, - \( T_1 = 100^\circ C \), \( T_2 = 0^\circ C \), - \( T \) is the temperature at the interface.
Step 2: Applying Given Ratio
Given that the ratio of thermal conductivities is: \[ K_{{brass}} : K_{{copper}} = 1:4. \] Let \( K_{{brass}} = K \) and \( K_{{copper}} = 4K \). Using the steady-state heat transfer equation: \[ \frac{4K (100 - T)}{d} = \frac{K (T - 0)}{d}. \] Step 3: Solving for Interface Temperature
Canceling \( K \) and \( d \): \[ 4 (100 - T) = T. \] \[ 400 - 4T = T. \] \[ 400 = 5T. \] \[ T = 80^\circ C. \] Step 4: Conclusion
Thus, the temperature at the interface is: \[ 80^\circ C. \]
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