廣瀬, 直喜, 中道, 二郎, Hirose, Naoki, Nakamichi, Jiro
航空宇宙技術研究所特別資料: 航空宇宙数値シミュレーション技術シンポジウム2001論文集 = Special Publication of National Aerospace Laboratory: Proceedings of Aerospace Numerical Simulation Symposium 2001
53
143-145,
2002-01
...Problem A is to compute the flow at free stream conditions of Mach number, 0.84, Reynolds number, 1 x 10(exp 6) and angle of attack, a = -1 deg, with free transition condition....
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