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解析的方法による航空機全機周りの計算格子生成
https://jaxa.repo.nii.ac.jp/records/43250
https://jaxa.repo.nii.ac.jp/records/432506f612be9-c23a-4bb3-98dc-d4391763a935
名前 / ファイル | ライセンス | アクション |
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nalsp0007034.pdf (480.1 kB)
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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 | 解析的方法による航空機全機周りの計算格子生成 | |||||
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 | Analytical Method for Generating Computational Grids about Complete Aircraft Configurations | |||||
著者 |
高梨, 進
× 高梨, 進× 伊沢, 隆男× Takanashi, Susumu× Isawa, Takao |
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著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
日本タイムシェア株式会社 | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
Nippon Time Share Co. | ||||||
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特別資料 en : Special Publication of National Aerospace Laboratory SP-7 巻 7, p. 281-288, 発行日 1986-12 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A method for constructing boundary-fitted grids for realistic aircraft configurations is described in this paper. The present grid generation procedure is based on the successive use of Caughey's wind tunnel mapping. The major advantage of the method is that the whole flow field can be transformed into a single rectangular computational domain, even for complex geometries such as that of the ONERA M-5 model. Typical examples of nearly orthogonal grid systems hitherto obtained are also presented. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0289-260X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN10097345 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: NALSP0007034 | |||||
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 SP-7 |