Two-Dimensional Modeling of Ablation and Pyrolysis with Application to Rocket Nozzles
Author:
Affiliation:
1. Naval Air Warfare Center Weapons Division, China Lake, California 93555
2. University of Michigan, Ann Arbor, Michigan 48109
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A33656
Reference37 articles.
1. Chemical Erosion of Carbon-Phenolic Rocket Nozzles with Finite-Rate Surface Chemistry
2. Carbon-Carbon Nozzle Erosion and Shape-Change Effects in Full-Scale Solid-Rocket Motors
3. Coupled Analysis of Flow and Surface Ablation in Carbon-Carbon Rocket Nozzles
4. Coupled Flow Field Simulations of Charring Ablators with Nonequilibrium Surface Chemistry
5. Computation of Multi-Dimensional Material Response Coupled to Hypersonic Flow
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