National Aerospace Laboratory
National Aerospace Laboratory
National Aerospace Laboratory
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-10
巻
10
ページ
59 - 64
発行年
1989-11
抄録（英）
An upwind scheme is constructed by the use of the eigenvalues and eigenvectors of the convective Jacobian matrices for the general non-equilibrium gas-dynamic equations in generalized curvilinear coordinates. This method is applied to chemically reacting hypersonic flows around a hemi-sphere cylinder and a spaceplane. The results show a splendid shock capturing capability and robustness of our scheme, revealing some characteristics of high temperature effects.
3次元再突入物体回りの反応流の計算
nalsp0010010.pdf
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