Correction to the Spalart–Allmaras Turbulence Model, Providing More Accurate Skin Friction
Author:
Affiliation:
1. Boeing Commercial Airplanes, Seattle, Washington 98124
2. Peter the Great St. Petersburg Polytechnic University, 195220, St. Petersburg, Russia
Funder
The Boeing Company
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference11 articles.
1. ColesD. E. “The Turbulent Boundary Layer in a Compressible Fluid,” RAND Rept. R403-PR, ARC 24473, California Institute of Technology, Pasadena, 1962, Appendix A.
2. Direct simulation of a turbulent boundary layer up to Rθ = 1410
3. Two-equation eddy-viscosity turbulence models for engineering applications
4. CebeciT.SmithA. M. O., Analysis of Turbulent Boundary Layers, Academic Press, New York, 1974, pp. 211–257.
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