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  2. 紀要論文 (Departmental Bulletin Paper)
  1. 機関資料(JAXA, former ISAS, NAL, NASDA)
  2. 旧機関資料 (JAXA, former-ISAS, NAL, NASDA)
  3. 宇宙科学研究所: ISAS Report等を含む (former ISAS (The Institute of Space and Astronautical Science): Including ISAS Report etc.)
  4. The Institute of Space and Astronautical Science report

Effect of the Flow Non-uniformity on the Mixing Layer at the Interface of Parallel Supersonic Flows

https://jaxa.repo.nii.ac.jp/records/31413
https://jaxa.repo.nii.ac.jp/records/31413
72511af1-10ca-4204-ba2d-411f1b524e43
名前 / ファイル ライセンス アクション
SA0035143.pdf SA0035143.pdf (797.0 kB)
Item type 紀要論文 / Departmental Bulletin Paper(1)
公開日 2015-03-26
タイトル
タイトル Effect of the Flow Non-uniformity on the Mixing Layer at the Interface of Parallel Supersonic Flows
言語 en
言語
言語 eng
資源タイプ
資源タイプ識別子 http://purl.org/coar/resource_type/c_6501
資源タイプ departmental bulletin paper
著者 ABE, Takashi

× ABE, Takashi

en ABE, Takashi

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FUNABIKI, Katsushi

× FUNABIKI, Katsushi

en FUNABIKI, Katsushi

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ARIGA, Hironobu

× ARIGA, Hironobu

en ARIGA, Hironobu

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HIRAOKA, Katsumi

× HIRAOKA, Katsumi

en HIRAOKA, Katsumi

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著者所属(英)
en
Institute of Space and Astronautical Science.
著者所属(英)
en
Institute of Space and Astronautical Science.
著者所属(英)
en
Musashi Institute of Technology.
著者所属(英)
en
School of Engineering, Tokai University.
出版者
出版者 宇宙科学研究所
出版者(英)
出版者 Institute of Space and Astronautical Science
書誌情報 en : The Institute of Space and Astronautical Science report

巻 646, p. 1-17, 発行日 1992-06
抄録(英)
内容記述タイプ Other
内容記述 The effect of flow non-uniformity on the supersonic mixing layer was investigated. The mixing layer is formed at the interface between the parallel supersonic flows of air and helium. The mixing layer was directly investigated by measuring the concentration ratio of helium. As for the flow non-uniformity, the stream-wise pressure gradient and the shock wave penetrating the mixing layer were considered. The effect of the stream-wise pressure gradient enhances the mixing rate by around 2 times in comparison with the one of the mixing layer without the effect. The shock impingement further enhances the mixing rate in comparison with the one of the mixing layer with the stream-wise pressure gradient but without the shock impingement. The enhancement of the mixing layer growth rate caused by the flow non-uniformities is attributed to the vorticity enhancement at the mixing layer, for which the baroclinic torque is a strong candidate.
ISSN
収録物識別子タイプ ISSN
収録物識別子 0285-6808
書誌レコードID
収録物識別子タイプ NCID
収録物識別子 AA10632072
資料番号
内容記述タイプ Other
内容記述 資料番号: SA0035143000
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