Stability-Based Transition Transport Modeling for Unstructured Computational Fluid Dynamics at Transonic Conditions
Author:
Affiliation:
1. DLR, German Aerospace Center, 37073 Göttingen, Germany
2. DLR, German Aerospace Center, 38108 Braunschweig, Germany
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J059892
Reference55 articles.
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3. ArnalD. “Boundary Layer Transition: Predictions Based on Linear Theory,” AGARD, Special Course on Progress in Transition Modelling 63, Rept. SEE N94-33884 10-34, 1993.
4. RANS modeling of high-speed aerodynamic flow transition with consideration of stability theory
5. Computational Fluid Dynamics Validation Issues in Transition Modeling
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