@inproceedings{oai:jaxa.repo.nii.ac.jp:00005786,
 author = {牧野, 好和 and Jeong, Shinkyu and 鈴木, 健一郎 and 上田, 良稲 and 松島, 紀佐 and 吉田, 憲司 and Makino, Yoshikazu and Jeong, Shinkyu and Suzuki, Kenichiro and Ueda, Yoshine and Matsushima, Kisa and Yoshida, Kenji},
 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, The aerodynamic design of an SST (SuperSonic Transport) configuration with some geometry requests at given flight condition in 3rd NAL-SST-CFD (Computational Fluid Dynamics) workshop competition subject 1 is conducted by following three design tools: a conventional linear theory design tool, a CFD-based optimization tool and a CFD-based inverse design tool. In order to increase a Lift to Drag ratio (L/D) of the airplane, several design concepts are adopted such as a warp wing design, linear and non-linear area-ruled fuselage designs and a supersonic NLF (Natural Laminar Flow) wing design. The non-linear area-ruled fuselage design shows that the CFD-based optimization design tool can improve the aerodynamic properties of the airplane designed by the conventional linear theory design tool. As for the NLF wing design, however, the CFD-based inverse design tool should be carefully coordinated in order to realize the target NLF pressure distributions., 資料番号: AA0063609055, レポート番号: JAXA-SP-06-029E},
 pages = {439--448},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {Optimized design},
 volume = {JAXA-SP-06-029E},
 year = {2007}
}