National Aerospace Laboratory
Nippon Time Share Co.
出版者
航空宇宙技術研究所
出版者（英）
National Aerospace Laboratory(NAL)
雑誌名
航空宇宙技術研究所特別資料
雑誌名(英)
Special Publication of National Aerospace Laboratory SP-7
巻
7
ページ
281 - 288
発行年
1986-12
抄録（英）
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.
解析的方法による航空機全機周りの計算格子生成
nalsp0007034.pdf
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