Nonequilibrium Surface Interactions Ablation Modeling with the Fully Implicit Ablation and Thermal Response Program
Author:
Affiliation:
1. University of Maryland
2. University of Colorado
3. Johns Hopkins University Applied Physics Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-1224
Reference32 articles.
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2. Heatshielding problems of planetary entry - A review
3. 4Park, Chul, and Yoon, Seokkwan, "A Fully-Coupled Implicit Method for Thermo-Chemical Nonequilibrium Air at Sub-Orbital Flight Speeds,"AIAAPaper, 89-1974, June1989.
4. Ablation and Thermal Response Program for Spacecraft Heatshield Analysis
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