@inproceedings{oai:jaxa.repo.nii.ac.jp:00038061,
 author = {廣瀬, 直喜 and 中道, 二郎 and Hirose, Naoki and Nakamichi, Jiro},
 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 = {There were four applicant teams for the present workshop. Because of time span between the announcement and the workshop was short to conduct full computation for three-D aircraft configuration even now, only one applicant presented the complete set of cases. The remaining teams presented some of the problems or trial case. After the workshop they are working on to complete analysis and will present their results in near future which will be put on the CFD on Web. In this compendium, because of this, a general survey look on the applicants analyses is presented. As a conclusion, it was found that three-D aircraft simulation is not so easy task to obtain reasonable data comparable to wind tunnel testing for aeronautical design., 資料番号: AA0032819025, レポート番号: NAL SP-53},
 pages = {146--148},
 publisher = {航空宇宙技術研究所, National Aerospace Laboratory (NAL)},
 title = {ワークショップ.ONERA M5全機形態まわりの流れの解析:結果の纏め},
 volume = {53},
 year = {2002}
}