@techreport{oai:jaxa.repo.nii.ac.jp:00043363,
 author = {柳沢, 三憲 and 中舘, 正顕 and 越岡, 康弘 and 井上, 敦 and Yanagizawa, Mitsunori and Nakadate, Masaaki and Koshioka, Yasuhiro and Inoue, Atushi},
 month = {Nov},
 note = {A computational procedure for generating three-dimensional grids around wing-fuselage configurations is presented. Resort is made of Green's theorm to obtain the required solution using of the panel methodology. Then the lines of force and equipotential surfaces surrounding the configuration determine a body-conforming orthogonal grid. Application of the method to several test cases shows that the grid for a fore-body is made smooth and continuous and that the grid for a civil transport plane is created. A finite-volume Euler solver is adapted to the grid system. Computed invisicid compressible flow solutions about the civil transport plane are presented., 資料番号: NALSP0010034, レポート番号: NAL SP-10},
 title = {境界要素法による三次元格子の生成},
 year = {1989}
}