@inproceedings{oai:jaxa.repo.nii.ac.jp:00005425,
 author = {高戸谷, 健 and 笠原, 利行 and 千葉, 一永 and 牧野, 好和 and Takatoya, Takeshi and Kasahara, Toshiyuki and Chiba, Kazuhisa and Makino, Yoshikazu},
 book = {宇宙航空研究開発機構特別資料: 第40回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2008論文集, JAXA Special Publication: Proceedings fo 40th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2008},
 month = {Feb},
 note = {第40回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2008. 会期: 2008年6月12日-6月13日. 会場: 東北大学片平キャンパス, For the wing shape design of supersonic technology demonstrator, multidisciplinary design exploration has been performed among aerodynamics, structures and sonic-boom noise. The structure evaluation was focused in this report. Evaluations of the composite structure were carried out by using a general finite element code, MSC/NASTRAN for strength, vibration and flutter requirements. The stacking sequences of the composite structures were set the design parameters to be determined for minimization of the structure weight in this multi-objective optimization problem., 形態: カラー図版あり, 資料番号: AA0064303023, レポート番号: JAXA-SP-08-009},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {静粛超音速研究機の多目的最適形状設計: 構造関連},
 volume = {JAXA-SP-08-009},
 year = {2009}
}