SOLUTION OF THE BOUNDARY-LAYER EQUATIONS FOR INCOMPRESSIBLE TURBULENT FLOW by A. M. 0. ... The existence of these two regions is due to the different response to shear and pressure gradient by the fluid near the wall. ... Engineer /Scientist Specialist, respectively, Aerodynamics Research Group, McDonnell Douglas Corporation, Douglas Aircraft Company, Long Beach, California.
|Title||:||Proceedings of the 1968 Heat Transfer and Fluid Mechanics Institute|
|Author||:||Heat Transfer and Fluid Mechanics Institute|
|Publisher||:||Stanford University Press - 1968|