@inproceedings{oai:jaxa.repo.nii.ac.jp:00038262,
 author = {山脇, るり子 and 児玉, 秀和 and 大庭, 芳則 and 山方, 章弘 and 野崎, 理 and 西澤, 敏雄 and 山本, 一臣 and Yamawaki, Ruriko and Kodama, Hidekazu and Oba, Yoshinori and Yamagata, Akihiro and Nozaki, Osamu and Nishizawa, Toshio and Yamamoto, Kazuomi},
 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 = {Recently, CFD analyses have been extensively applied to noise reduction technologies of a supersonic transport engine. This paper introduces the CFD activities for noise reduction technologies. For fan noise, the magnitude of unsteady pressure on the 3D stator vane evaluated through a use of unsteady 3D stage analysis. For jet noise, Large Eddy Simulation (LES) is applied to prediction of exhaust jet mixing of a lobed mixer nozzle. It is confirmed that a CFD application takes an important role in noise reduction technologies., 資料番号: AA0045948041, レポート番号: NAL SP-57},
 pages = {232--237},
 publisher = {航空宇宙技術研究所, National Aerospace Laboratory (NAL)},
 title = {超音速輸送機用エンジン低騒音化技術への数値流体解析の適用},
 volume = {57},
 year = {2003}
}