@techreport{oai:jaxa.repo.nii.ac.jp:00043256,
 author = {小川, 哲 and 石黒, 登美子 and 高倉, 葉子 and Ogawa, Satoru and Ishiguro, Tomiko and Takakura, Yoko},
 month = {Nov},
 note = {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., 資料番号: NALSP0008003, レポート番号: NAL SP-8},
 title = {飛翔体まわり流れの数値計算},
 year = {1987}
}