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Unsteady shock wave motions on a thin airfoil at transonic speeds caused by aileron oscillations

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玉山, 雅人, 中道, 二郎, Tamayama, Masato, Nakamichi, Jiro宇宙航空研究開発機構2004-03-25宇宙航空研究開発機構研究開発報告 = JAXA Research and Development ReportJAXA-RR-03-017E

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Subject Heading...low shock wave thin airfoil aileron oscillation boundary ...

ワークショップ翼型失速特性シミュレーション.結果のまとめ:CFDは翼型失速角を予測できるか?

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廣瀬, 直喜, 中橋, 和博, 吉田, 憲司, 松尾, 裕一, 岩宮, 敏幸, Hirose, Naoki, Nakahashi, Kazuhiro, Yoshida, Kenji, Matsuo, Yuichi, Iwamiya, Toshiyuki航空宇宙技術研究所2000-12航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory46p.175-177

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Subject Heading...characteristic thin airfoil separation
Note (General)...all. As for A3 thin airfoil, they also obtained various r...

ワークショップ翼型失速特性シミュレーション2DST-6:CFDは翼型失速角を予測できるか

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松島, 紀佐, 岩宮, 敏幸, Matsushima, Kisa, Iwamiya, Toshiyuki航空宇宙技術研究所2000-12航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory46p.147-150

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Subject Heading...ing edge stall thin airfoil stall turbulence model Navier...
Note (General)...dge stall, and thin airfoil stall. There are three well-k...

CFDは翼型失速角を予測できるか?:乱流モデルの比較

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松本, 崇, Matsumoto, Takashi航空宇宙技術研究所2000-12航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory46p.123-128

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Subject Heading...dge stall type thin airfoil stall turbulence model aircra...

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