Numerical Investigation of Fluid-Ablation Interactions for a Mach 5.3 Transitional Boundary Layer Flow Over a 13 Degree Cone
Author:
Affiliation:
1. University of Maryland at College Park
2. University of Kentucky
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2023-0476
Reference31 articles.
1. Decoupling ablation effects on boundary-layer stability and transition
2. Real-Gas and Surface-Ablation Effects on Hypersonic Boundary-Layer Instability over a Blunt Cone
3. Analysis of Ablation on Boundary Layer Stability of the Reentry F Flight Vehicle
4. Treviño, L. "Numerical Simulation of Surface Patterns on Sublimating Ablative Materials," Ph.D. thesis,University of Minnesota, Minneapolis, Minnesota, 052021.
5. Cross-Hatching — An Interaction between Shock and Turbulent Boundary Layer
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