RANS Closure Model Assessment using LES /RANS Datasets for a Hypersonic Crossing-Shock Interaction
Author:
Affiliation:
1. North Carolina State University
2. Oak Ridge National Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-0590
Reference15 articles.
1. Two-equation eddy-viscosity turbulence models for engineering applications
2. RANS and LES Simulation of a Mach 7 Axisymmetric Flare Interaction
3. Evaluation of RANS Closure Models using LES Datasets for Hypersonic Shock Boundary Layer Interactions
4. A Computational Analysis of Ground Test Studies of the HIFiRE-1 Transition Experiment
5. The Lag Model Applied to High Speed Flows
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1. Data-Driven RANS Modeling of Hypersonic Shock / Boundary Layer Interactions;AIAA SCITECH 2024 Forum;2024-01-04
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