Ablation Model Based on Porous Charring Layer Under Alumina Erosion Condition
Author:
Affiliation:
1. Northwestern Polytechnical University, 710072 Xi’an, People’s Republic of China
2. State Key Laboratory of Clean Energy Utilization, Zhejiang University, 310027 Hangzhou, People’s Republic of China
Funder
National Natural Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference30 articles.
1. Flow Inside a Solid Rocket Motor with Relation to Nozzle Inlet Ablation
2. Insulator ablation modes in different impact conditions of alumina droplets onto wall surfaces
3. Inhomogeneity in pore size appreciably lowering thermal conductivity for porous thermal insulators
4. KooJ. H.LinS.KneerM. “Comparison of Ablative Materials in a Simulated Solid Rocket Exhaust Environment,” AIAA Paper 1991-0978, 1991.
5. YangB. C.CheungF. B.KooJ. H. “Numerical Investigation of Thermo-Chemical and Mechanical Erosion of Ablative Materials,” AIAA Paper 1993-2045, 1993.
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