Hypersonic Ablation of Graphite Thermal Protection Systems with Surface Defects
Author:
Affiliation:
1. The University of Akron, Akron, Ohio 44325-3903
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A33380
Reference45 articles.
1. Comparison of Hertz-Knudsen and Ytrehus Carbon Ablation Rates Using a Reactive-Riemann Solver
2. Modeling of Local Intense Ablation in Hypersonic Flight
3. Dynamics of Plumes Generated by Local Injection of Ablated Material
4. Computational Aerothermodynamic Design Issues for Hypersonic Vehicles
5. Ablation and Thermal Response Property Model Validation for Phenolic Impregnated Carbon Ablator
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