@inproceedings{oai:jaxa.repo.nii.ac.jp:00038258,
 author = {佐々木, 大輔 and Yang, Guowei and 大林, 茂 and Sasaki, Daisuke and Yang, Guowei and Obayashi, Shigeru},
 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2002論文集, Special Publication of National Aerospace Laboratory: Proceedings of Aerospace Numerical Simulation Symposium 2002},
 month = {Mar},
 note = {In this research, multiobjective optimization system has been developed to reduce the aerodynamic drag and the sonic boom for SST wing-body configuration. Wing and fuselage are defined by 131 design variables and optimized at the same time. 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 boom is evaluated based on the equivalent area distribution by Darden. MOGA is used as an optimizer of the present optimization. To reduce the large computation time, CFD computations are parallelized by a simple master-slave concept on SGI ORIGIN 2000 at The Institute of Fluid Science at Tohoku University., 資料番号: AA0045948037, レポート番号: NAL SP-57},
 pages = {208--213},
 publisher = {航空宇宙技術研究所, National Aerospace Laboratory (NAL)},
 title = {多目的最適化によるソニックブームと空力抵抗のトレードオフ解探索},
 volume = {57},
 year = {2003}
}