@techreport{oai:jaxa.repo.nii.ac.jp:00045154,
 author = {石黒, 登美子 and 小川, 哲 and 小口, 慶子 and ISHIGURO, Tomiko and OGAWA, Satoru and OGUCHI, Keiko},
 month = {Dec},
 note = {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., 資料番号: NALTR0896000, レポート番号: NAL TR-896},
 title = {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},
 year = {1985}
}