Experimental Evaluation of Inductively Coupled Plasma Flow Analysis Code
Author:
Affiliation:
1. Japan Aerospace Exploration Agency
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-175
Reference11 articles.
1. Ito, T.,Kurotaki, T.,Matsuzaki, T.,Ishida,K.andWatanabe,Y.:EvaluationofSurfaceCatalytic Effecton TPS in Arc-heatedWindTunnel,AIAApaper2002-3335,2002.
2. Ito, T., Kurotaki, T., Sumi, T., Fujita, K., Mizuno, M., and Ishida, K.: Evaluation of Surface Catalytic Effect on TPSin110kWICP-heatedWind Tunnel,AIAApaper2005-0189,2005.
3. Energy Partitions in Inductively Heated Plasma Sources for Reentry Simulations
4. Vanden Abeele, D. and Degrez, G.: Numerical Model of High-Pressure Air Inductive Plasmas under Thermal and ChemicalNon-Equilibrium, AIAApaper2000-2416,2000.
5. Fujita, K., Mizuno, M., Ishida, K., Ito, T., Sumi, T. and Kurotaki, T.: Spectroscopic Diagnostics of Electrically HeatedHighEnthalpyWindTunnels,AIAApaper2005-0173,2005.
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