Detailed Information

Cited 0 time in webofscience Cited 0 time in scopus
Metadata Downloads

Effect of neutral pressure on the He plasma flow measurement in a linear device

Full metadata record
DC Field Value Language
dc.contributor.authorPark, Eun-Kyong-
dc.contributor.authorWoo, Hyun-Jong-
dc.contributor.authorChung, Kyu Sun-
dc.contributor.authorTanaka, Hirohiko-
dc.contributor.authorKajita, Shin-
dc.contributor.authorOhno, Noriyasu-
dc.date.accessioned2022-07-16T12:56:57Z-
dc.date.available2022-07-16T12:56:57Z-
dc.date.issued2012-11-
dc.identifier.issn1567-1739-
dc.identifier.issn1878-1675-
dc.identifier.urihttps://scholarworks.bwise.kr/hanyang/handle/2021.sw.hanyang/164296-
dc.description.abstractAxial and azimuthal flow velocities have been measured in a linear plasma device called NAGDIS-II (NAGoya DIvertor Simulator-II), along with plasma density and electron temperature, using a vector Mach probe composed of two Mach probes, one of which is for the axial flow, and the other is for the azimuthal flow. To study the effect of neutral pressure on the deduction of the Mach numbers, the ratio of upstream to downstream currents are measured by changing the neutral pressure for the deduction of flow velocities. Helium plasma was generated with pressure of 2-35 mTorr. Since the ion gyro-radius at the magnetic flux of 300 G is larger than the probe size, an unmagnetized collisionless Mach probe theory was used for the deduction of Mach numbers and their variations. In order to check the range of collisionality, plasma density (n(e) = 10(10)-10(11) cm(-3)) and electron temperature (T-e 2-9 eV) are measured by a single electric probe using a conventional collisionless probe theory. Variations of Mach number, electron temperature and plasma density with collisionless models are to be compared with those using collisional models for different pressures where ionization and ion-neutral collision are included. Mach numbers by the collisionless model are found to be overestimated by 120% for the maximum difference even in weakly collisional plasmas. A clear flow reversal exists in the axial direction with higher pressure plasma, even in the linear machine. Azimuthal flows are also measured simultaneously along with axial flows, yet they seem to be very small in the present cold ion plasma (T-i/T-e << 1).-
dc.format.extent6-
dc.language영어-
dc.language.isoENG-
dc.publisherThe Korean Physical Society-
dc.titleEffect of neutral pressure on the He plasma flow measurement in a linear device-
dc.typeArticle-
dc.publisher.location대한민국-
dc.identifier.doi10.1016/j.cap.2012.04.024-
dc.identifier.scopusid2-s2.0-84863980697-
dc.identifier.wosid000306420500016-
dc.identifier.bibliographicCitationCurrent Applied Physics, v.12, no.6, pp 1497 - 1502-
dc.citation.titleCurrent Applied Physics-
dc.citation.volume12-
dc.citation.number6-
dc.citation.startPage1497-
dc.citation.endPage1502-
dc.type.docTypeArticle-
dc.identifier.kciidART001756347-
dc.description.isOpenAccessN-
dc.description.journalRegisteredClasssci-
dc.description.journalRegisteredClassscie-
dc.description.journalRegisteredClassscopus-
dc.description.journalRegisteredClasskci-
dc.relation.journalResearchAreaMaterials Science-
dc.relation.journalResearchAreaPhysics-
dc.relation.journalWebOfScienceCategoryMaterials Science, Multidisciplinary-
dc.relation.journalWebOfScienceCategoryPhysics, Applied-
dc.subject.keywordPlusION COLLECTION-
dc.subject.keywordPlusEDGE PLASMA-
dc.subject.keywordPlusKINETIC-THEORY-
dc.subject.keywordPlusMACH PROBE-
dc.subject.keywordPlusVISCOSITY-
dc.subject.keywordPlusVELOCITY-
dc.subject.keywordPlusDIVERTOR-
dc.subject.keywordPlusTOKAMAK-
dc.subject.keywordAuthorPlasma flow-
dc.subject.keywordAuthorUnmagnetized Mach probe-
dc.subject.keywordAuthorIon-neutral collision-
dc.subject.keywordAuthorDivertor simulator-
dc.subject.keywordAuthorHelium plasma-
dc.identifier.urlhttps://www.sciencedirect.com/science/article/pii/S1567173912001630?via%3Dihub-
Files in This Item
Go to Link
Appears in
Collections
서울 공과대학 > 서울 전기공학전공 > 1. Journal Articles

qrcode

Items in ScholarWorks are protected by copyright, with all rights reserved, unless otherwise indicated.

Altmetrics

Total Views & Downloads

BROWSE