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  1. 機関資料(JAXA, former ISAS, NAL, NASDA)
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  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.)
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An approximate Numerical Approach to Separated Flows at Transonic Speeds

https://jaxa.repo.nii.ac.jp/records/34573
https://jaxa.repo.nii.ac.jp/records/34573
386402dd-3c54-4c3c-a2c7-325bc1b3c1ec
名前 / ファイル ライセンス アクション
SA2401444.pdf SA2401444.pdf (1.0 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 An approximate Numerical Approach to Separated Flows at Transonic 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 FUJII, Kozo

× FUJII, Kozo

en FUJII, Kozo

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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 46, 号 7, p. 209-228, 発行日 1981-03
抄録(英)
内容記述タイプ Other
内容記述 A numerical method for solving the transonic viscous-inviscid flow interaction is newly developed. The finite difference equations derived from the basic equations for viscous and inviscid flows and the coupling condition between them constitute a system of nonlinear simultaneous equations having a tridiagonal coefficient matrix at each longitudinal station, which can be easily solved using SLOR method. The process is just like that of inviscid flow calculations except that the unknown column vector at each station includes three boundary layer variables. Solutions for the inviscid flow and the boundary layer are obtained simultaneously without any difficulty. The method is applied to the flow over a divergent wall and a circular-arc airfoil respectively, where separation and/or wake flow pattern may appear. Calculations are executed for several cases of Reynolds numbers and Mach numbers. In order to demonstrate the applicability of the present approach, the results are compared with the experimental and another numerical ones and the effects of the various parameters on the interaction phenomenon are examined.
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: SA2401444000
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