Investigation of an equilibrium condition boundary layer in front of a material probe in a subsonic plasma flow-Reference-Cited by-同舟云学术

Investigation of an equilibrium condition boundary layer in front of a material probe in a subsonic plasma flow

Published:1996-06-17 Issue: Volume: Page:
ISSN:
Container-title:31st Thermophysics Conference
language:
Short-container-title:

Author:

Winter M.¹,Auweter-Kurtz M.¹,Kurtz H.¹,Park C.²

Affiliation:

1. Stuttgart, Univ., Germany

2. Tohoku Univ., Sendai, Japan

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1996-1853

Reference7 articles.

1. Auweter-Kurtz, M., Kurtz, H.L. and Laure, S. "Plasma Generators for Re-entry Simulation", Internal Report IRS-95-IB10, Institut fur Raumfahrtsysteme, Universitat Stuttgart, Stuttgart, Germany, 1995.

2. Auweter-Kurtz, M., Friiholz, H., Habiger, H., Stockle, Th. and Hilfer, G. "Comparison of a magnetoplasmadynamic and a thermal plasma wind tunnel as tools for the investigation of heatshield materials for space transportation systems", Internal Report IRS-95-P10, Institut fur Raumfahrtsysteme, Universitat Stuttgart, Stuttgart, Germany, 1995.

3. Spectroscopic determination of enthalpy in an arc-jet wind tunnel

4. Assessment of two-temperature kinetic model for ionizing air

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