Numerical Simulations of Multiscale Ablation of Carbon/Carbon Throat with Morphology Effects
Author:
Affiliation:
1. Northwestern Polytechnical University, 710072 Xi’an, People’s Republic of China
2. Beijing Suansheng Technologies Co., Ltd., 100600 Beijing, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J055534
Reference29 articles.
1. Aerothermochemical analysis of carbon-carbon nozzle regression in solid-propellant rocket motors
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3. Mechanical Erosion of Graphite Nozzle in Solid-Propellant Rocket Motor
4. Flow Inside a Solid Rocket Motor with Relation to Nozzle Inlet Ablation
5. HIGH-TEMPERATURE BEHAVIOR OF GRAPHITE UNDER LASER IRRADIATION
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4. Coupled Thermo-Structural Analysis Model of Solid Rocket Motor Nozzle considering the Variation of Friction Coefficient under Operating Conditions;International Journal of Aerospace Engineering;2022-02-21
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