@inproceedings{oai:jaxa.repo.nii.ac.jp:00037835,
 author = {松本, 崇 and 山内, 豊誠 and 越岡, 康弘 and 清島, 哲 and Matsumoto, Takashi and Yamauchi, Toyosei and Koshioka, Yasuhiro and Kiyoshima, Satosi},
 book = {航空宇宙技術研究所特別資料, Special Publication of National Aerospace Laboratory},
 month = {Dec},
 note = {非平衡層流であるOREXのまわりの2次元軸対称極超音速流を数値的に計算した。強い衝撃波を含む極超音速流を安定に解くために、Roeの流束差分分割法に基く風上差分解法を採用した。気体の解離･再結合を取り扱うためParkの5種モデルを利用した。計算結果は、強い衝撃波の下流側における非平衡現象を明瞭に示す。, A two dimensional axisymmetric hypersonic flow around Orbital Reentry Experiment (OREX), that consist of non-equilibrium laminar flow, was solved numerically. Roe's flux difference splitting upwind technique was adopted to solve the hypersonic flow that contains strong shock stably. To treat dissociating-recombinating gas phenomena, Park's five-species model was utilized. The numerical result shows non-equilibrium gas phenomena behind the strong shock clearly., 資料番号: AA0004173011, レポート番号: NAL SP-26},
 pages = {67--70},
 publisher = {航空宇宙技術研究所, National Aerospace Laboratory (NAL)},
 title = {2次元軸対称OREX回りの非平衡流の計算},
 volume = {26},
 year = {1994}
}