Development of a Langmuir probe for plasma diagnostic work in high speed flow

Author:

Menart J.1,Shang J.2,Hayes J.2

Affiliation:

1. Wright State Univ., Dayton, OH

2. USAF, Research Lab., Wright-Patterson AFB, OH

Publisher

American Institute of Aeronautics and Astronautics

Reference28 articles.

1. Magnetohydrodynamic-Hypersonic Flow Past a Blunt Body

2. Shang, J. S., Canupp, P. W., and Gaitonde, D. V, "Computational magneto-aerodynamic hypersonics," AIAA paper #99-4903,

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3. DC Plasma Discharge Effects on a Mach 5 Flow Between Small Plate Electrodes;35th AIAA Plasmadynamics and Lasers Conference;2004-06-20

4. Data Reduction Analysis for a Cylindrical, Double Langmuir Probe Operating in a High Speed Flow;42nd AIAA Aerospace Sciences Meeting and Exhibit;2004-01-05

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