Calculation of Incompressible Turbulent Boundary Layers With Mass Transfer, Including Highly Accelerating Flows

[+] Author and Article Information
T. Cebeci, G. J. Mosinskis

Aerodynamics Research Group, Douglas Aircraft Co., McDonnell Douglas Corp., Long Beach, Calif.

J. Heat Transfer 93(3), 271-280 (Aug 01, 1971) (10 pages) doi:10.1115/1.3449811 History: Received March 31, 1970; Revised October 29, 1970; Online August 11, 2010


This paper describes a general method for calculating turbulent boundary layers with and without mass addition. The method, as in earlier studies, is based on the eddy-viscosity concept. However, the eddy-viscosity formulation presented in this paper differs from the previous ones in that the previous eddy-viscosity formulation has been generalized to handle flows with mass transfer. A large number of flows computed with this method show good agreement with experiment.

Copyright © 1971 by ASME
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