Computer Center, National Aerospace Laboratory(NAL)
Computer Center, National Aerospace Laboratory(NAL)
Computer Center, National Aerospace Laboratory(NAL)
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報告
雑誌名(英)
Technical Report of National Aerospace Laboratory TR-896
巻
896
ページ
10
発行年
1985-12
抄録（英）
The main purpose of this paper is to numerically analyse inviscid flows about wing-fuselage combinations. In the third series we present a numerical procedure for calculating flows based on the Euler equations by the finite volume method using the Runge-Kutta type scheme and the local time stepping technique. The grids, which have already been generated by the code YOKUDO-G in the first series, are used in the calculations. Many examples are presented to show the utility of this numerical procedure for flows about several wing-fuselage combinations. Numerical results obtained by this procedure are compared with experimental results and the numerical results obtained using the full potential equation in the second series.
翼胴結合体まわり非粘性圧縮流の数値解析 Ⅲ.Euler方程式による計算
naltr00896.pdf
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