Wind-US Code Physical Modeling Improvements to Complement Hypersonic Testing and Evaluation
Author:
Affiliation:
1. NASA Glenn Research Center
2. Embry Riddle Aeronautical University
3. AEDC/ATA
4. ITAC
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-193
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5. Turbulence Model Predictions of Strongly Curved Flow in a U-Duct
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