The determination of turbulent length scales in algebraic turbulencemodels for attached and slightly separated flows using Navier-Stokesmethods
Author:
Affiliation:
1. Dornier GmbH, Friedrichshafen, West Germany
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1987-1302
Reference25 articles.
1. 'Marvin, 1.G."Turbulence Modeling for Computational Aerodynamics," AIAA-Paper 82-164 (1982)
2. 3Baldwin, B.S., Lomax, H. "Thin Layer Approximation and Algebraic Model for Separated Turbulent Flows," AIAA-Paper 78-257 (1978)
3. 4Visbal, M. Knight, D. "Evaluation of the Baldwin-Lomax Turbulence Model for Two-Dimensional Shock Wave Boundary Layer Interactions," AIAAPaper 83-1697 (1983)
4. The law of the wake in the turbulent boundary layer
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