Investigation of Freestream Plasma Flow Produced by Inductively Coupled Plasma Wind Tunnel
Author:
Affiliation:
1. Information Engineering Department, Second University of Naples, 81031 Aversa, Italy
2. Aeronautics and Aerospace Department, von Kármán Institute for Fluid Dynamics, B-1640 Rhode-Saint-Genèse, Belgium
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.T4199
Reference34 articles.
1. PaneraiF. “Aerothermochemistry Characterization of Thermal Protection Systems,” Ph.D. Dissertation, Aeronautics and Aerospace Dept. von Kármán Inst. for Fluid Dynamics, Rhode-Saint-Genèse, Belgium, 2012.
2. On Catalytic Recombination Rates in Hypersonic Stagnation Heat Transfer
3. Flight Extrapolation of Plasma Wind Tunnel Stagnation Region Flowfield
4. Comparison of Enthalpy Determination Methods for an Arc-Jet Facility
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