論文

査読有り 本文へのリンクあり
2017年10月16日

Plasma-Assisted Control of Mach-2 Flowfield over Ramp Geometry

IOP Conference Series: Materials Science and Engineering
  • Yasumasa Watanabe
  • ,
  • Sergey B. Leonov
  • ,
  • Alec Houpt
  • ,
  • Brock E. Hedlund
  • ,
  • Skye Elliott

249
1
記述言語
英語
掲載種別
研究論文(国際会議プロシーディングス)
DOI
10.1088/1757-899X/249/1/012006
出版者・発行元
IOP PUBLISHING LTD

© 2017 Published under licence by IOP Publishing Ltd. This study examined the effect of Reynolds number on plasma-assisted flow control ahead of a compression ramp geometry in Mach-2 supersonic flow. The experiments were conducted in the supersonic wind tunnel SBR-50 at the University of Notre Dame. Stagnation temperature and pressure were varied as T0=294-500K and P0=1-3bar to attain Reynolds number ranging from 3.4×105-2.2×106. Ramp pressure measurements, schlieren visualization, and high-speed camera imaging were used for the evaluation of plasma-assisted flow control effects. A linear dependency was found between the ramp pressure change per averaged plasma power and Reynolds number.

Web of Science ® 被引用回数 : 2

リンク情報
DOI
https://doi.org/10.1088/1757-899X/249/1/012006
Web of Science
https://gateway.webofknowledge.com/gateway/Gateway.cgi?GWVersion=2&SrcAuth=JSTA_CEL&SrcApp=J_Gate_JST&DestLinkType=FullRecord&KeyUT=WOS:000419294700006&DestApp=WOS_CPL
Scopus
https://www.scopus.com/inward/record.uri?partnerID=HzOxMe3b&scp=85034252652&origin=inward 本文へのリンクあり
Scopus Citedby
https://www.scopus.com/inward/citedby.uri?partnerID=HzOxMe3b&scp=85034252652&origin=inward
ID情報
  • DOI : 10.1088/1757-899X/249/1/012006
  • ISSN : 1757-8981
  • eISSN : 1757-899X
  • SCOPUS ID : 85034252652
  • Web of Science ID : WOS:000419294700006

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