WEKO3
アイテム
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高レイノルズ数遷音速流翼型解析プログラムNSFOILの開発
https://jaxa.repo.nii.ac.jp/records/45074
https://jaxa.repo.nii.ac.jp/records/4507467bf8a97-7764-4949-922a-5b7765992743
名前 / ファイル | ライセンス | アクション |
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naltr00816.pdf (1.7 MB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 高レイノルズ数遷音速流翼型解析プログラムNSFOILの開発 | |||||
言語 | ||||||
言語 | jpn | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Development of the Code NSFOIL for Analizing High Reynolds Number Transonic Flow around an Airfoil | |||||
著者 |
河合, 伸坦
× 河合, 伸坦× 廣瀬, 直喜× KAWAI, Nobuhiro× HIROSE, Naoki |
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著者所属 | ||||||
航空宇宙技術研究所空気力学第二部 | ||||||
著者所属 | ||||||
航空宇宙技術研究所空気力学第二部 | ||||||
著者所属(英) | ||||||
en | ||||||
Second Aerodynamics Division, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Second Aerodynamics Division, National Aerospace Laboratory(NAL) | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory(NAL) | |||||
書誌情報 |
航空宇宙技術研究所報告 en : Technical Report of National Aerospace Laboratory TR-816 巻 816, p. 20, 発行日 1984-06 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A computer code, called NSFOIL, has been developed for analyzing high Reynolds number transonic flow around an airfoil. The implicit approximate factorization scheme for the Navier-Stokes (NS) equations with an algebraic eddy viscosity model of the turbulent boundary layer is used with the implicit boundary condition on the airfoil and the wake cut boundary. The present code contains various option parameters for physical models, and I/O forms, i.e., full or thin layer approximate NS equations, fully turbulent or transition models of boundary layer, etc. Emphasis is put on the various output forms of the computed results to provide aerodynamics designers with full information on aerodynamic, boundary layer and wake characteristics including shock-induced separation and trailing edge separation phenomena. Some of the computed results are presented and compared with the wind tunnel experiment results. In the appendix, the operation manual of the code is described. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0389-4010 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: NALTR0816000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL TR-816 |