Multidimensional Finite Volume Fully Implicit Ablation and Thermal Response Code
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, California 94035-0001
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.A34184
Reference17 articles.
1. Ablation and Thermal Response Program for Spacecraft Heatshield Analysis
2. Effects of Nonequilibrium Chemistry and Darcy—Forchheimer Pyrolysis Flow for Charring Ablator
3. Ablation, Thermal Response, and Chemistry Program for Analysis of Thermal Protection Systems
4. Multidimensional Effects on Heatshield Thermal Response for the Orion Crew Module
5. Two-Dimensional Implicit Thermal Response and Ablation Program for Charring Materials
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