Implicit Coupling Approach for Simulation of Charring Carbon Ablators
Author:
Affiliation:
1. Thermal Protection Materials Branch, NASA Ames Research Center, Moffett Field, California 94035-1000
2. ERC, Inc., Moffett Field, California 94035-1000
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.A32753
Reference24 articles.
1. Loosely Coupled Simulation for Two-Dimensional Ablation and Shape Change
2. Computational Analysis of Arc-Jet Stagnation Tests Including Ablation and Shape Change
3. Data-Parallel Line Relaxation Method for the Navier-Stokes Equations
4. Two-Dimensional Implicit Thermal Response and Ablation Program for Charring Materials
5. Effect of Surface Nonequilibrium Thermochemistry in Simulation of Carbon Based Ablators
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