Improved Large-Eddy Simulation Validation Methodology: Application to Supersonic Inlet/Isolator Flow
Author:
Affiliation:
1. Department of Aerospace Engineering and Engineering Mechanics, The University of Texas at Austin, Austin, Texas 78712
2. Flight Vehicle Research Center, Seoul National University, Seoul 151-744, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J053049
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