المؤلفون: Iwamiya, Toshiyuki, Yoshida, Kenji, Shinbo, Yuichi, Makino, Yoshikazu, Matsushima, Kisa

المصدر: 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). :274-279

مصطلحات موضوعية: aerodynamical design, 超音速機, National Experimental Supersonic Transport, arrow type planform, 計算流体力学, computational fluid dynamics, 自然層流翼, ねじれ翼, 航空機設計, boundary layer transition, aircraft design, 境界層遷移, NEXST, 空力設計, 超音速実験機, 胴翼構成, area ruled fuselage, 圧力分布, design optimization, research aircraft, 実験機, pressure distribution, 設計最適化, body-wing configuration, aerodynamic design, 矢羽根平面型, warped wing, aerodynamic characteristic, wing planform, supersonic experimental airplane, 翼平面形, 小型超音速実験機計画, 空力特性, CFD, natural laminar flow wing, supersonic aircraft, 面積則胴体

URL الوصول: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::66df18c4d3ae9dcbc771a42dec6fecdc
http://id.nii.ac.jp/1696/00005755/

Additional Titles: 超音速実験機の空力設計

المؤلفون: Iwamiya, Toshiyuki, Yoshida, Kenji, Shinbo, Yuichi, Makino, Yoshikazu, Matsushima, Kisa, 岩宮 敏幸, 吉田 憲司, 真保 雄一, 牧野 好和, 松島 紀佐

مصطلحات الفهرس: supersonic experimental airplane, aerodynamical design, natural laminar flow wing, CFD, computational fluid dynamics, NEXST, National Experimental Supersonic Transport, arrow type planform, warped wing, area ruled fuselage, 超音速実験機, 空力設計, 自然層流翼, 計算流体力学, 小型超音速実験機計画, 矢羽根平面型, ねじれ翼, 面積則胴体, Technical Report, jaxa, 航空宇宙技術研究所