@inproceedings{oai:jaxa.repo.nii.ac.jp:00006465,
 author = {Jeong, Shinkyu and 金崎, 雅博 and 村山, 光宏 and Jeong, Shinkyu and Kanazaki, Masahiro and Murayama, Mitsuhiro},
 book = {宇宙航空研究開発機構特別資料: 航空宇宙数値シミュレーション技術シンポジウム2004論文集, JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2004},
 month = {Mar},
 note = {In this study, Kriging model is applied to an aerodynamic design of a high lift device. The position of a slat and a flap is optimized. The Kriging model is updated by selection of the maximum EI point. Sample points for the Kriging model are evaluated by using UPACS (Unified Platform for Aerospace Computational Simulation) multi-block solver developed in JAXA. The effect of each position parameter to the aerodynamic performance can be identified by 3D-plot of the Kriging model., 資料番号: AA0048469025, レポート番号: JAXA-SP-04-012},
 pages = {151--154},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {High lift device optimization design with Kriging model},
 volume = {JAXA-SP-04-012},
 year = {2005}
}