National Aerospace Laboratory
National Aerospace Laboratory
National Aerospace Laboratory
Fujitsu Limited.
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-16
巻
16
ページ
21 - 26
発行年
1991-12
抄録（英）
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.
複合格子による数値計算
nalsp0016004.pdf
(1.39MB)
