Numerical Analysis of Graphite Ablation in Nitrogen Flow
Author:
Affiliation:
1. Japan Aerospace Exploration Agency
2. Nagoya University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-1217
Reference17 articles.
1. Unified Calculation of Hypersonic Flowfield for a Reentry Vehicle
2. Calculation of Thermal Response of Ablator Under Arcjet Flow Condition
3. The carbon-atomic oxygen reaction—surface-oxide formation on paracrystalline carbon and graphite
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1. An introduction to the derivation of surface balance equations without the excruciating pain;International Journal of Heat and Mass Transfer;2017-12
2. Experimental Study of Graphite Ablation in Nitrogen Flow;Journal of Thermophysics and Heat Transfer;2008-07
3. Comprehensive Characterization of Test Flows in 110-kW Inductively-Coupled-Plasma Heater;46th AIAA Aerospace Sciences Meeting and Exhibit;2008-01-07
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