Multiphysics Coupled Fluid/Thermal/Ablation Simulation of Carbon/Carbon Composites
Author:
Affiliation:
1. Harbin Institute of Technology, 150080 Harbin, People’s Republic of China
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.A33612
Reference29 articles.
1. Performance of a Low Density Ablative Heat Shield Material
2. Hypersonic-finite rate chemically reacting viscous flows over an ablating carbon surface
3. Development of a Nonequilibrium Finite-Rate Ablation Model for Radiating Earth Reentry Flows
4. Two-Dimensional Implicit Thermal Response and Ablation Program for Charring Materials
5. Predictions of Ablating Hypersonic Vehicles Using an Iterative Coupled Fluid/Thermal Approach
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