Stability-Based Transition Model Using Transport Equations
Author:
Affiliation:
1. ONERA–University of Toulouse, F-31055 Toulouse, France
2. Airbus Operations SAS, 31060 Toulouse, France
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference34 articles.
1. Correlation-Based Transition Modeling for Unstructured Parallelized Computational Fluid Dynamics Codes
2. Extending the Gamma-Rethetat Correlation based Transition Model for Crossflow Effects (Invited)
3. Transport Modeling for the Prediction of Crossflow Transition
4. Computational Fluid Dynamics Compatible Transition Modeling Using an Amplification Factor Transport Equation
5. Van IngenJ. L. “A Suggested Semi-Empirical Method for the Calculation of the Boundary Layer Transition Region,” Delft Univ. of Technology Tech. Rept. VTH-74, Dept. of Aerospace Engineering, Delft, the Netherlands, 1956.
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