@inproceedings{oai:jaxa.repo.nii.ac.jp:00005403,
 author = {渡辺, 悠人 and 三坂, 孝志 and 大林, 茂 and 加藤, 琢真 and 齋木, 祐一郎 and 有馬, 敏幸 and 山口, 義博 and Watanabe, Yuto and Misaka, Takashi and Obayashi, Shigeru and Kato, Takuma and Saiki, Yuichiro and Arima, Toshiyuki and Yamaguchi, Yoshihiro},
 book = {宇宙航空研究開発機構特別資料: 第40回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2008論文集, JAXA Special Publication: Proceedings fo 40th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2008},
 month = {Feb},
 note = {第40回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2008. 会期: 2008年6月12日-6月13日. 会場: 東北大学片平キャンパス, The gamma-Re(sub theta) transition model was applied to predict the boundary layer transition on NACA0015 airfoil and validated by comparing the simulation results with experiment. The comparison showed the lack of prediction accuracy in negative pressure gradient. The crossflow parameter proposed by Kohama et al. was selected as a candidate for crossflow modeling and its implementation was attempted only using local flow variables. The crossflow parameter was evaluated on the flowfield of S5010 swept wing and compared with other crossflow parameters. The results showed the potential effectiveness of this criterion., 形態: カラー図版あり, 資料番号: AA0064303001, レポート番号: JAXA-SP-08-009},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {γ-Re(sub θ)遷移モデルの検証と横流れ不安定のモデル化に関する検討},
 volume = {JAXA-SP-08-009},
 year = {2009}
}