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Computation on collisionless steady-state plasma flow past a charged diskA computer method is presented using the 'inside-out' approach, for predicting the structure of the disturbed zone near a moving body in space. The approach uses fewer simplifying assumptions than other available methods, and is applicable to large ranges of the values of body and plasma parameters. Two major advances concerning 3-dimensional bodies are that thermal motions of ions as well as of electrons are treated realistically by following their trajectories in the electric field, and the technique for achieving self-consistency is promising for very large bodies. Three sample solutions were obtained for a disk-shaped body, charged negatively to a potential 4kT/e. With ion Mach number 4, and equal ion and electron temperatures, the wakes of a relatively small body (radius 5 Debye lengths) and a relatively large body (radius 100 Debye lengths) both begin to fill up between 2 and 3 body radii downstream. For the large body there is in addition a potential well (about 6kT/e deep) behind the body. Increasing the ion Mach number to 8 for the large body causes the potential well to become wider and longer but not deeper. For the large body, the quasineutrality assumption is validated outside of a cone-shaped region in the very near wake. For the large as well as the small body, the disturbed zone behind the body extends transversely no more than 2 or 3 body radii, a result of significance for the design of spacecraft boom instrumentation.
Document ID
19760011843
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Parker, L. W.
(Parker (Lee W.), Inc. Concord, MA, United States)
Date Acquired
September 3, 2013
Publication Date
February 1, 1976
Subject Category
Plasma Physics
Report/Patent Number
NASA-CR-144159
Report Number: NASA-CR-144159
Accession Number
76N18931
Funding Number(s)
CONTRACT_GRANT: NASA ORDER H-16314-B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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