@techreport{oai:jaxa.repo.nii.ac.jp:00043500,
 author = {小川, 哲 and 和田, 安弘 and 石黒, 登美子 and 高倉, 葉子 and Ogawa, Satoru and Wada, Yasuhiro and Ishiguro, Tomiko and Takakura, Yoko},
 month = {Dec},
 note = {The multi-domain technique is used to solve the whole flowfields around the combined configuration of space vehicles. Several computational grids are overlapped with each other in the computational domain, and the solutions are combined by the interpolation scheme at the boundary of each grid. The TVD scheme of finite volume and post-processing type is used to solve the Navier-Stokes equations for hypersonic flow. The numerical computations are performed for two problems, i.e., NASA space shuttle/external tank roket booster and NANDA HOPE/H2 roket/roket boosters, and it is shown the results of numerical simulation using the present methods are reasonable., 資料番号: NALSP0016004, レポート番号: NAL SP-16},
 title = {複合格子による数値計算},
 year = {1991}
}