Wall Function Boundary Conditions Including Heat Transfer and Compressibility
Author:
Affiliation:
1. University of Alabama in Birmingham, Birmingham, Alabama 35294
2. Jacobs Sverdrup Arnold Engineering Development Center Group, Arnold Air Force Base, Tennessee 37389
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.3539
Reference17 articles.
1. A First Course in Turbulence
2. Development and validation of a two-equation turbulence model with wall functions for compressible flow
3. On the use of wall functions as boundary conditions for two-dimensional separated compressible flows
4. The k-kl turbulence model and wall layer model for compressible flows
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