Recent Developments in Calculation Methods for Turbulent Boundary Layers With Pressure Gradients and Heat Transfer

[+] Author and Article Information
J. C. Rotta

Aerodynamische Versuchsanstalt, Goettingen, Germany

J. Appl. Mech 33(2), 429-437 (Jun 01, 1966) (9 pages) doi:10.1115/1.3625061 History: Received March 11, 1965; Online September 15, 2011


A review is given of the recent development in turbulent boundary layers. At first, for the case of incompressible flow, the variation of the shape of velocity profile with the pressure gradient is discussed; also the temperature distribution and heat transfer in incompressible boundary layers are treated. Finally, problems of the turbulent boundary layer in compressible flow are considered.

Copyright © 1966 by ASME
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