@inproceedings{oai:jaxa.repo.nii.ac.jp:00005787,
 author = {佐々木, 大輔 and Yang, Guowei and 大林, 茂 and Sasaki, Daisuke and Yang, Guowei and Obayashi, Shigeru},
 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, In this research, multiobjective optimization system has been developed to reduce the aerodynamic drag and the sonic boom for SST (SuperSonic Transport) wing-body configuration. Wing and fuselage are defined by 131 design variables and optimized at the same time. Structured multiblock grids around SST wing-body configuration are generated automatically and an Euler solver is used to evaluate the aerodynamic performance of SST wing-body configuration., 資料番号: AA0063609056, レポート番号: JAXA-SP-06-029E},
 pages = {449--454},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {Automated aerodynamic design optimization system for SST wing-body configuration},
 volume = {JAXA-SP-06-029E},
 year = {2007}
}