Error versus y+ for Three Turbulence Models: Incompressible Flow Over a Unit Flat Plate
Author:
Affiliation:
1. U. S. Army Aviation & Missile RDEC
2. University of Alabama in Huntsville
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2007-3968
Reference22 articles.
1. rensk ., McKeel , S. A., and Papay, M . L. "Comp arison of E ngineering and CFD Predictions and WindTunnel Data fora Launch Vehicle Configuration," AIAA Paper 1997-2251.
2. Dillenius, M. F. E., Lesieutre, D. J, Hegedus, M. C., Perkins, S. C. Jr., Love, J. F., and Lesieutre, T. O. "Engineering, Intermediate,and High Level Aerodynamic PredictionMethodsand Applications," AIAA Paper1997-2278.
3. Srivastava,B."CFDAnalysisandValidationofLateralJetControlofaMissile,"AIAAPaper96-0288.
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