المؤلفون: Takasawa, Kingo

المصدر: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory. 37:1-8

مصطلحات موضوعية: aerodynamic configuration, 数値流体力学, lift to drag ratio, wing body configuration, 超音速輸送機, computational fluid dynamics, 揚力係数, クリーン形態実験機, subscaled unmanned supersonic experimental aircraft, 線形理論, linear theory, supersonic transport, 揚抗比, airframe structure design, 翼面荷重, SST, 機体構造設計, wing surface pressure distribution, 縮尺無人超音速実験機, 翼面圧力分布, lift coefficient, wing load, 翼胴形状, CFD, clean configuration experimental aircraft, 空力形状

URL الوصول: https://explore.openaire.eu/search/publication?articleId=jairo_______::d18e1a774d2f6ec942f43c547d72c48a
http://id.nii.ac.jp/1696/00037121/

المؤلفون: Iwamiya, Toshiyuki, Ogawa, Satoru

المصدر: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory. 36:109-112

مصطلحات موضوعية: supersonic transport, 数値流体力学, lift drag ratio, 揚抗比, computational fluid dynamics, aerodynamic design technology, aircraft configuration, 空力設計技術, 超音速無人実験機, ジェットエンジン推進航空機, unmanned supersonic experimental aircraft, 航空機形状, ロケット実験機, jet engine propelled aircraft, integration design technology, turbulence research, 統合設計技術, 乱流研究, rocket engine launched aircraft, 超音速旅客機

URL الوصول: https://explore.openaire.eu/search/publication?articleId=jairo_______::9e42cf79c5c89b922c7be8e64cc0bd85
http://id.nii.ac.jp/1696/00037111/

Additional Titles: System design of scaled high-speed experimental aircraft and roles of CFD

المؤلفون: Takasawa, Kingo, 高澤 金吾

مصطلحات الفهرس: SST, supersonic transport, subscaled unmanned supersonic experimental aircraft, aerodynamic configuration, wing body configuration, CFD, computational fluid dynamics, lift coefficient, lift to drag ratio, linear theory, wing load, wing surface pressure distribution, airframe structure design, clean configuration experimental aircraft, 超音速輸送機, 縮尺無人超音速実験機, 空力形状, 翼胴形状, 数値流体力学, 揚力係数, 揚抗比, 線形理論, 翼面荷重, 翼面圧力分布, 機体構造設計, クリーン形態実験機, Conference Paper, jaxa, 航空宇宙技術研究所