Feasibility study for analyzing plasma-aerodynamic effects Metadata
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Title
- Main Title Feasibility study for analyzing plasma-aerodynamic effects
Creator
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Author: Penetrante, BCreator Type: Personal
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Author: Sherohman, JCreator Type: Personal
Contributor
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Sponsor: United States. Department of Energy. Office of the Assistant Secretary for Defense Programs.Contributor Type: OrganizationContributor Info: USDOE Office of Defense Programs (DP)
Publisher
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Name: Lawrence Livermore National LaboratoryPlace of Publication: Livermore, CaliforniaAdditional Info: Lawrence Livermore National Laboratory (LLNL), Livermore, CA
Date
- Creation: 1999-05-07
Language
- English
Description
- Content Description: The purpose of this feasibility study was to conduct preliminary modeling to elucidate the mechanisms responsible for the effects observed in the Air Force Research Laboratory (AFRL) shock tube experiment. It was assumed that the plasma is simply a region of gas in the shock tube that has a higher gas temperature. Computational fluid dynamics (CFD) calculations were performed to simulate the propagation of a shock wave through the tube, using the same parameters in the experiment. Both 1- D and 3-D CFD calculations were performed to determine which effects can be explained simply by axial temperature gradients and which effects require the presence of radial temperature gradients. Discharge plasma physics calculations of a longitudinal glow discharge were then used to establish if the electrical currents used in the experiment are consistent with the gas temperature distributions that are necessary to explain the observed effects.
- Physical Description: 155 Kilobytes
Subject
- Keyword: Aerodynamics
- Keyword: Feasibility Studies
- STI Subject Categories: 66 Physics
- Keyword: Plasma
Collection
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Name: Office of Scientific & Technical Information Technical ReportsCode: OSTI
Institution
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Name: UNT Libraries Government Documents DepartmentCode: UNTGD
Resource Type
- Report
Format
- Text
Identifier
- Other: DE00007951
- Report No.: UCRL-ID-133912
- Grant Number: W-7405-Eng-48
- DOI: 10.2172/7951
- Office of Scientific & Technical Information Report Number: 7951
- Archival Resource Key: ark:/67531/metadc740975