Data-Driven RANS Modeling of Hypersonic Shock / Boundary Layer Interactions
Author:
Affiliation:
1. Sandia National Laboratories
2. NC State University
3. Oak Ridge National Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2024-2736
Reference25 articles.
1. Two-equation eddy-viscosity turbulence models for engineering applications
2. A Computational Analysis of Ground Test Studies of the HIFiRE-1 Transition Experiment
3. The Lag Model Applied to High Speed Flows
4. Revisiting Turbulence Model Validation for High-Mach Number Axisymmetric Compression Corner Flows
5. RANS and LES Simulation of a Mach 7 Axisymmetric Flare Interaction
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