Application of Linear and Nonlinear Two-Equation Turbulence Models in Hypersonic Flows
Author:
Affiliation:
1. State Key Laboratory of Aerodynamics, 621000 Mianyang, People’s Republic of China
2. University of Manchester, Manchester, M13 9PL, United Kingdom
Funder
National Key Research and Development Plan of China
National Natural Science Foundation of China
National Numerical Wind Tunnel Project of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J061077
Reference25 articles.
1. Fifty Years of Shock-Wave/Boundary-Layer Interaction Research: What Next?
2. Review and assessment of turbulence models for hypersonic flows
3. CoakleyT. J.HorstmanC. C.MarvinJ. G.ViegasJ. R.BardinaJ. E.HuangP. G.KussoyM. I. “Turbulence Compressibility Corrections,” NASA TM 108827, 1994.
4. RubesinM. W. “Extra Compressibility Terms for Favre-Averaged Two-Equation Models of Inhomogeneous Turbulent Flows,” NASA CR 177556, June 1990.
5. Turbulence models for compressible boundary layers
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