Characteristics of a Supersonic Plasma Flow in a Magnetic Nozzle.
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- INUTAKE Masaaki
- Department of Electrical Engineering, Tohoku University
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- ANDO Akira
- Department of Electrical Engineering, Tohoku University
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- HATTORI Kunihiko
- Department of Electrical Engineering, Tohoku University
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- TOBARI Hiroyuki
- Department of Electrical Engineering, Tohoku University
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- YAGAI Tsuyoshi
- Department of Electrical Engineering, Tohoku University
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Abstract
A high-density and high-speed flowing helium-plasma is produced quasi-steadily (1 ms) by use of a magneto-plasma-dynamic arcjet (MPDA) in various external magnetic field configurations. In a uniform magnetic field configuration, an ion acoustic Mach number Mi of the plasma flow is limited to be nearly unity. In a divergent magnetic nozzle configuration, on the other hand, the Mach number increases up to almost 3. The Mach number increases in proportion to the gradient of the magnetic field. Spatial variations of Mi are well predicted by an isentropic model of compressible flow. The Mach number decreases in the downstream region due to charge-exchange collisional processes that are caused by a limited pumping capability of surface-recombined neutral gases.
Journal
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- Journal of Plasma and Fusion Research
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Journal of Plasma and Fusion Research 78 (12), 1352-1360, 2002
The Japan Society of Plasma Science and Nuclear Fusion Research
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Details 詳細情報について
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- CRID
- 1390001206513108224
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- NII Article ID
- 130000133612
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- NII Book ID
- AN10401672
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- COI
- 1:CAS:528:DC%2BD3sXhsVGmu7k%3D
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- NDL BIB ID
- 6422184
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- ISSN
- 09187928
- http://id.crossref.org/issn/09187928
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- Text Lang
- en
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- Data Source
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- JaLC
- NDL
- Crossref
- CiNii Articles
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- Abstract License Flag
- Disallowed