@inproceedings{oai:jaxa.repo.nii.ac.jp:00017369,
 author = {下山, 幸治 and 藤井, 孝藏 and 小林, 弘明 and Shimoyama, Koji and Fujii, Kozo and Kobayashi, Hiroaki},
 book = {宇宙輸送シンポジウム　平成14年度, Proceedings of Space Transportation Symposium FY2002},
 month = {Apr},
 note = {A new aerodynamics model is developed using the data obtained by accurate CFD simulations, as one of the components for the total optimization of TSTO systems. The developed component is integrated into the optimization program, and the influence of the new component is evaluated. Strong aerodynamic interaction occurs between the Booster and the Orbiter in the CFD simulations, and it indicates the importance of the accurate aerodynamics model. The optimization using the new aerodynamics model results in the heavier gross take-off weight compared to the result using the conventional aerodynamics model., 資料番号: AA0045426033},
 pages = {133--136},
 title = {TSTO統合最適設計の高度化:CFD解析によるTSTO空力評価モデルの構築},
 year = {2003}
}