Immersed-Boundary Wall-Modeled Large-Eddy Simulation of High Mach Number Boundary Layer Flows
Author:
Affiliation:
1. University of Oxford
2. University of Kentucky, Lexington
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2021-2751
Reference40 articles.
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4. 4LeVeque, R. J., Time-Split Methods for Partial Differential Equations, Ph.D. thesis,Stanford University, 1982.
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