National Aerospace Laboratory
National Aerospace Laboratory
Fujitsu Ltd.
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-8
巻
8
ページ
19 - 28
発行年
1987-11
抄録（英）
Numerical simulations of flow around shuttle orbiter are performed by solving the 3-dimensional Euler equations. A numerical grid is generated for the whole configuration of shuttle orbiter by using equations of mesh line orthogonality and cell volume which form a hyperbolic partial differential equation system. To increase the applicability of the hyperbolic grid generation scheme, the second metric tensor is used for the determination of cell volume, and the one-dimensional elastic model is used to relax the orthogonality condition of two coordinate lines. The transonic and supersonic flows around the shuttle orbiter are solved by using the Harten-Yee type TVD scheme. It is shown the results of numerical flow simulation using the present methods is reasonable.
飛翔体まわり流れの数値計算
nalsp0008003.pdf
(977.34KB)
