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An investigation of non-equilibrium effects in an argon free-jet plasma

Citation

Cassady, Phillip Earl (1970) An investigation of non-equilibrium effects in an argon free-jet plasma. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/WHYP-RZ81. https://resolver.caltech.edu/CaltechTHESIS:10012010-092851271

Abstract

The non-equilibrium effects present in the formation of a strong normal shock wave in a low density, slightly ionized argon flow field, particularly as evidenced by the appearance of a dark region upstream of the shock wave, have been analyzed both theoretically and experimentally. A model for the flow through the shock wave was formulated which incorporates a quantum mechanical theory to explain the existence of the dark region, and the problem was solved numerically to yield flow field property distributions. A precursor region of high electron temperature was found to exist upstream of the main body of the heavy-particle shock wave. An experimental investigation of the phenomenon was carried out in an arc heated free jet flow field. A test facility was constructed in which the goal has been to attain operation at low enough enthalpies to allow precise and extensive diagnostic testing while still high enough to exhibit the interesting non-equilibrium effects. Extensive study was carried out on the effect of electrode design and gas flow phenomena on the stability of the arc discharge. The completed unit was instrumented fully for measurement of the operating parameters and a computer program was developed to monitor its operation as a supply of slightly ionized argon for free-jet experiments. The non-equilibrium aspects of the free-jet were analyzed both theoretically and experimentally. A theoretical model was developed and numerically solved for the free-jet expansion of slightly ionized argon. Pitot pressure measurements were completed and compared favorably with predictions calculated from this theoretical model. Electron temperature and ion density profiles were measured both along the axis of the empty free-jet and through the normal shock wave in front of a cooled blunt body using a new type of cooled Langmuir probe, the operation of which was theoretically analyzed. The existence of a region of electron temperature in front of a strong normal shock wave coincident with the observed dark region was experimentally verified.

Item Type:Thesis (Dissertation (Ph.D.))
Subject Keywords:Aeronautics
Degree Grantor:California Institute of Technology
Division:Engineering and Applied Science
Major Option:Aeronautics
Thesis Availability:Public (worldwide access)
Research Advisor(s):
  • Lees, Lester
Group:GALCIT
Thesis Committee:
  • Unknown, Unknown
Defense Date:10 February 1970
Funders:
Funding AgencyGrant Number
U.S. Army Research Office and Advanced Research Projects AgencyDA-31-124-ARO(D)-33
Record Number:CaltechTHESIS:10012010-092851271
Persistent URL:https://resolver.caltech.edu/CaltechTHESIS:10012010-092851271
DOI:10.7907/WHYP-RZ81
Default Usage Policy:No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:6083
Collection:CaltechTHESIS
Deposited By: Benjamin Perez
Deposited On:01 Oct 2010 18:06
Last Modified:21 Dec 2019 03:03

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