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  2. 紀要論文 (Departmental Bulletin Paper)
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The Flow Near the Region of Vertex of Axially Symmetric Bodies at Supersonic Speeds

https://jaxa.repo.nii.ac.jp/records/34381
https://jaxa.repo.nii.ac.jp/records/34381
076f52a3-e83e-4047-9cd8-f3b5ea65e994
名前 / ファイル ライセンス アクション
SA2400513.pdf SA2400513.pdf (1.8 MB)
Item type 紀要論文 / Departmental Bulletin Paper(1)
公開日 2015-03-26
タイトル
タイトル The Flow Near the Region of Vertex of Axially Symmetric Bodies at Supersonic Speeds
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 KARASHIMA, Keiichi

× KARASHIMA, Keiichi

en KARASHIMA, Keiichi

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出版者
出版者 東京大学宇宙航空研究所
出版者(英)
出版者 Institute of Space and Aeronautical Science,University of Tokyo
書誌情報 en : ISAS report/Institute of Space and Aeronautical Science,University of Tokyo

巻 31, 号 1, p. 1-30, 発行日 1966-02
抄録(英)
内容記述タイプ Other
内容記述 An analytical method for axially symmetric supersonic flow involving shock wave is presented and applied to clarify the characteristic feature of the flow near the region of vertex of the pointed bodies of revolution with arbitrary geometry. The method used in the present approach is exact except for an assumption that the flow is inviscid. It is shown that the present method can be further applied, with a slight modification, to a circular-cone with such large semi-vertex angle that the flow behind the shock wave is partially subsonic. Detailed examination reveals that in axially symmetric flow there exists a particular point which corresponds to Crocco point in plane flow and the flow characters near the region of vertex of the body are qualitatively quite the same as those of the plane flow. It is concluded that the transition from attached to detached shock wave is continuous for circular-cones as well as for plane wedges.
ISSN
収録物識別子タイプ ISSN
収録物識別子 0372-1418
書誌レコードID
収録物識別子タイプ NCID
収録物識別子 AA00675986
資料番号
内容記述タイプ Other
内容記述 資料番号: SA2400513000
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