@inproceedings{oai:jaxa.repo.nii.ac.jp:00005789,
 author = {吉本, 稔 and 海田, 武司 and Yoshimoto, Minoru and Kaiden, Takeshi},
 book = {宇宙航空研究開発機構特別資料, JAXA Special Publication: Proceedings of International Workshops on Numerical Simulation Technology for Design of Next Generation Supersonic Civil Transport (SST-CFD Workshop)},
 month = {Mar},
 note = {SST-CFDワークショップ.次世代超音速機の数値シミュレーション利用技術に関する国際ワークショップ 航空宇宙技術研究所 20011203-20011205 東京 日本, SST-CFD Workshop. International Workshops on Numerical Simulation Technology for Design of Next Generation Supersonic Civil Transport National Aerospace Laboratory 20011203-20011205 Tokyo Japan, CFD (Computational Fluid Dynamics) analyses of flow around NAL's non-powered supersonic experimental airplane are conducted. The results are compared with those of corresponding wind tunnel tests. In this paper, agreements and discrepancies between them are discussed in aspects of correspondence between calculation and test models., 資料番号: AA0063609058, レポート番号: JAXA-SP-06-029E},
 pages = {468--473},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {Numerical simulations of flow around NAL's non-powered supersonic experimental airplane},
 volume = {JAXA-SP-06-029E},
 year = {2007}
}