Table 9.1 shows the numerical results obtained from Blasius exact solution of the laminar boundary-layer equations. Plot the velocity distribution (note that from Eq. 9.13 we see that η  5:0 y δ). On...

Table 9.1 shows the numerical results obtained from

Blasius exact solution of the laminar boundary-layer equations. Plot the velocity distribution (note that from Eq. 9.13

we see that η  5:0 y

δ). On the same graph, plot the turbulent

velocity distribution given by the 1

7-power expression of

Eq. 9.24. Which is most likely to separate first when

encountering an adverse pressure gradient? To justify your

answer, compare the momentum fluxes of these profiles (the

laminar data can be integrated using a numerical method

such as Simpson’s rule).