Computational Framework for Coupling Compressible and Low Mach Number Codes
Author:
Affiliation:
1. Stanford University, Stanford, California 94305
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.32884
Reference26 articles.
1. A Framework for Coupling Reynolds-Averaged With Large-Eddy Simulations for Gas Turbine Applications
2. Integrated Computations of an Entire Jet Engine
3. Peet, Y. "Film Cooling from Inclined Cylindrical Holes Using Large Eddy Simulations," Ph.D. Thesis,Dept. of Aeronautics and Astronautics, Stanford Univ., Stanford, CA,2006.
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