Experimental Study of Graphite Ablation in Nitrogen Flow, Part II: Further Numerical Analysis
Author:
Affiliation:
1. Japan Aerospace Exploration Agency, Tokyo 182-0012, Japan
2. Nagoya University, Aichi 464-8603, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Condensed Matter Physics,Aerospace Engineering,Space and Planetary Science,Fluid Flow and Transfer Processes,Mechanical Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.43264
Reference11 articles.
1. Experimental Study of Graphite Ablation in Nitrogen Flow
2. Shock-Tube Measurement of Nitridation Coefficient of Solid Carbon
3. Calculation of Thermal Response of Ablator Under Arcjet Flow Condition
4. Comprehensive Flow Characterization in a 110-Kilowatt Inductively-Coupled-Plasma Heater
5. Application of integral methods to ablation charring erosion - A review
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