@inproceedings{oai:jaxa.repo.nii.ac.jp:00038065,
 author = {藤田, 健 and 伊藤, 靖 and 中橋, 和博 and 松島, 紀佐 and 岩宮, 敏幸 and Fujita, Takeshi and Ito, Yasushi and Nakahashi, Kazuhiro and Matsushima, Kisa and Iwamiya, Toshiyuki},
 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2001論文集, Special Publication of National Aerospace Laboratory: Proceedings of Aerospace Numerical Simulation Symposium 2001},
 month = {Jan},
 note = {Aerodynamic interference of airframe/engine integration of NAL jet experimental airplane is evaluated by solving the Euler equations on unstructured tetrahedral grids. Aerodynamic coefficients of C(sub L), C(sub D) and C(sub M) of Jet#08 configuration are compared for 11 cases by changing the nacelle position in the vertical direction. Each configuration with modified nacelle position is defined using CATIA. Owing to the close-coupled procedure from CAD modeling to surface meshing, all these evaluations can be performed within 3 days., 資料番号: AA0032819029, レポート番号: NAL SP-53},
 pages = {167--172},
 publisher = {航空宇宙技術研究所, National Aerospace Laboratory (NAL)},
 title = {CFDを用いたNAL　jet実験機におけるナセル干渉解析},
 volume = {53},
 year = {2002}
}