Parallel Compatible Transition Closure Model for High-Speed Transitional Flow
Author:
Affiliation:
1. Northwestern Polytechnical University, 710072 Xi’an, People’s Republic of China
2. Xi’an Jiaotong University, 701149 Xi’an, People’s Republic of China
3. Beihang University, 100191 Beijing, People’s Republic of China
Funder
National Basic Research Program of China
National Science Foundation for Young Scholars
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J055711
Reference46 articles.
1. Development of an Intermittency Equation for the Modeling of the Supersonic/Hypersonic Boundary Layer Flow Transition
2. MackL. M. “Transition Prediction and Linear Stability Theory,” AGARD CP-224, Neuilly sur Seine, France, 1977, pp. 1-1–1-22.
3. Transition model for high-speed flow
4. Transition Closure Model for Predicting Transition Onset
5. Transition Onset Prediction for High-Speed Flow
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