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Ion wind drag reductionIn order to study the effect of ion wind on viscous drag, the equations of electrogasdynamics are solved numerically assuming the flow is incompressible, the electric field is steady and that the fluid velocity is negligible compared to ion drift velocity. The results obtained to date in a continuing theoretical and experimental research program are presented.
Document ID
19830036696
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Malik, M. R. (High Technology Corp. Hampton, VA, United States)
Weinstein, L. M. (NASA Langley Research Center Hampton, VA, United States)
Hussaini, M. Y. (Institute for Computer Applications in Science and Engineering Hampton, VA, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1983
Subject Category
Plasma Physics
Report/Patent Number
AIAA PAPER 83-0231
Report Number: AIAA PAPER 83-0231
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting
Location: Reno, NV
Start Date: January 10, 1983
End Date: January 13, 1983
Accession Number
83A17914
Funding Number(s)
CONTRACT_GRANT: NAS1-16916
CONTRACT_GRANT: NAS1-16394
Distribution Limits
Public
Copyright
Other

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