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Numerical simulation of MPD thruster flows with anomalous transportAnomalous transport effects in an Ar self-field coaxial MPD thruster are presently studied by means of a fully 2D two-fluid numerical code; its calculations are extended to a range of typical operating conditions. An effort is made to compare the spatial distribution of the steady state flow and field properties and thruster power-dissipation values for simulation runs with and without anomalous transport. A conductivity law based on the nonlinear saturation of lower hybrid current-driven instability is used for the calculations. Anomalous-transport simulation runs have indicated that the resistivity in specific areas of the discharge is significantly higher than that calculated in classical runs.
Document ID
19920071517
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Caldo, Giuliano
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Choueiri, Edgar Y.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Kelly, Arnold J.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Jahn, Robert G.
(Princeton University NJ, United States)
Date Acquired
August 15, 2013
Publication Date
July 1, 1992
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 92-3738
Accession Number
92A54141
Funding Number(s)
CONTRACT_GRANT: AF-AFOSR-91-0162
CONTRACT_GRANT: NAS9-54997
Distribution Limits
Public
Copyright
Other

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