Investigation of Freestream Plasma Flow Produced by Inductively Coupled Plasma Wind Tunnel-Reference-Cited by-同舟云学术

Investigation of Freestream Plasma Flow Produced by Inductively Coupled Plasma Wind Tunnel

Published:2014-07 Issue:3 Volume:28 Page:381-393
ISSN:0887-8722
Container-title:Journal of Thermophysics and Heat Transfer
language:en
Short-container-title:Journal of Thermophysics and Heat Transfer

Author:

Cipullo Alessio¹,Helber Bernd²,Panerai Francesco²,Zeni Luigi¹,Chazot Olivier²

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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