@inproceedings{oai:jaxa.repo.nii.ac.jp:00005744,
 author = {鈴木, 亙 and 藤本, 朗 and 高須, 徹 and Suzuki, Wataru and Fujimoto, Akira and Takasu, Toru},
 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 Workshop. International CFD Workshops for Super-sonic Transport Design 航空宇宙技術研究所 19980316-19980317 東京 日本, SST-CFD Workshop. International CFD Workshops for Super-sonic Transport Design National Aerospace Laboratory 19980316-19980317 Tokyo Japan, SJAC (Society of Japanese Aerospace Companies) Phase-2 SST (SuperSonic Transport) configuration was designed by JADC (Japan Aircraft Development Corporation) SST working group. CFD (Computational Fluid Dynamics) analysis was conducted on the wing-body configuration to obtain preliminary aerodynamic data including non-linear effects such as transonic effect and so on, which are not counted in the primary design procedure. The results and the information obtained though this study are going to be discussed on this paper., 資料番号: AA0063609013, レポート番号: JAXA-SP-06-029E},
 pages = {84--87},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {Aerodynamic design of SJAC Phase-2 SST configuration},
 volume = {JAXA-SP-06-029E},
 year = {2007}
}