Consider the plane wall of Figure 3.1, separating hot and cold fluids at temperatures $T_{\infty, 1}$ and $T_{\infty, 2}$, respectively. Using surface energy balances as boundary conditions at $x=0$ and $x=L$ (see Equation 2.34), obtain the temperature distribution within the wall and the heat flux in terms of $T_{\infty, 1}, T_{\infty, 2}, h_{1}, h_{2}, k$, and $L$.