Using numerical results obtained by Blasius (Table 9.1), evaluate the vertical component of velocity in a laminar boundary layer on a flat plate. Plot v/U versus y/δ for Rex 5 105 . Verify that the y...

Using numerical results obtained by Blasius (Table 9.1),

evaluate the vertical component of velocity in a laminar

boundary layer on a flat plate. Plot v/U versus y/δ for Rex 5 105

.

Verify that the y component of velocity for the Blasius

solution to the Prandtl boundary-layer equations is given by

Eq. 9.10. Obtain an algebraic expression for the x component

of the acceleration of a fluid particle in the laminar boundary

layer. Plot ax versus η to determine the maximum x component of acceleration at a given x.