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Electrical conductivity and velocity of highly ionized plasma flows - Theory and experiment.Use of an immersible, three-coil, magnetic-induction probe, previously tested in a low-density supersonic argon jet, to measure electrical conductivity and velocity profiles of a highly ionized high-density nitrogen jet in the continuum flow regime where effects due to probe bow shocks and boundary layers might not be negligible. Measured centerline values of electrical conductivity and velocity were compared with predictions based on a theoretical analysis previously developed to study the gas as it expanded adiabatically and inviscidly from an equilibrium sonic state to the nozzle exit. The resulting numerical exit plane values for electron density and electron temperature were then substituted into the Spitzer-Haerm conductivity formula to compute a theoretical conductivity which agreed within 40% of the measured conductivity, while the calculated and experimental velocity values differed by as much as 50%. The lack of agreement was attributed to the possible use of invalid assumptions and boundary conditions in the computer analysis or to the unknown effects of shocks on the probe data.
Document ID
19720050403
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Vendell, E. W.
(Utah State University of Agriculture and Applied Science, Logan, Utah, United States)
Park, C.
(NASA Ames Research Center Moffett Field, Calif., United States)
Posch, R. E.
Date Acquired
August 6, 2013
Publication Date
June 1, 1972
Subject Category
Physics, Plasma
Report/Patent Number
AIAA PAPER 72-671
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Fluid and Plasma Dynamics Conference
Location: Boston, MA
Start Date: June 26, 1972
End Date: June 28, 1972
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
72A34069
Funding Number(s)
CONTRACT_GRANT: NGR-45-002-019
CONTRACT_GRANT: NASA USU-201
CONTRACT_GRANT: NGR-45-002-014
Distribution Limits
Public
Copyright
Other

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