@inproceedings{oai:jaxa.repo.nii.ac.jp:00038263,
 author = {西澤, 敏雄 and 才木, 一寿 and 野崎, 理 and 菊地, 一雄 and Nishizawa, Toshio and Saiki, Kazuhisa and Nozaki, Osamu and Kikuchi, Kazuo},
 book = {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2002論文集, Special Publication of National Aerospace Laboratory: Proceedings of Aerospace Numerical Simulation Symposium 2002},
 month = {Mar},
 note = {The computation is performed on a turbine stator blade with cooling air ejection from multi-row holes on the surface. This computation reveals the complicated three-dimensional structure in the stator passage including secondary flow and end-wall separation, and how the ejected cooling air flows on the blade surface and how the surface temperature is protected from the hot gas. The influence of the air ejection on the aerodynamic performance is also examined., 資料番号: AA0045948042, レポート番号: NAL SP-57},
 pages = {238--243},
 publisher = {航空宇宙技術研究所, National Aerospace Laboratory (NAL)},
 title = {フィルム冷却されたタービン翼列内流れの数値シミュレーション},
 volume = {57},
 year = {2003}
}