The boundary conditions that were used in developing the equation for the
laminar thermal boundary layer were that the temperature is known at the two
limits \((1) \theta=0\) at \(\eta=0\) and \((2) \theta=1\) at \(\eta \rightarrow\)
large. What would be the temperature distribution if the boundary conditions
were (1) an adiabatic wall (i.e., \(\theta^{\prime}=0\) at \(\eta=0\) ), and \((2)
\theta=1\) at \(\eta \rightarrow\) large? Hint: From equation \((4.97)\),
$$
\theta^{\prime}=C\left(f^{\prime \prime}\right)^{\mathrm{Fr}}
$$
