المؤلفون: Kheirandish, Hamid Reza, Nakamichi, Jiro

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). :366-369

مصطلحات موضوعية: 超音速機, dynamic pressure, transonic flight, 計算流体力学, computational fluid dynamics, 非定常オイラー方程式, structural design, 遷音速領域, フラッタ境界, 空力弾性応答, vibration damping, エルロンフラッタ, 航空機設計, フラッタ, フラッタ速度, 線形理論, 遷音速飛行, aircraft design, flutter boundary, linear theory, unsteady Euler equation, 振動減衰, transonic region, aeroelastic response, research aircraft, 実験機, 構造設計, SST, flutter speed, 数値シミュレーション, aileron flutter, flutter, 動圧, numerical simulation, SST experimental aircraft, SST実験機, supersonic aircraft

URL الوصول: https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::47031f46b6c13af92789ca45ae014c3f
http://id.nii.ac.jp/1696/00005768/

المؤلفون: Kheirandish, Hamid Reza, Nakamichi, Jiro

المصدر: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory. 41:41-46

مصطلحات موضوعية: thin layer Navier Stokes equation, supersonic transport, transonic wind tunnel, 数値流体力学, ADI形式, forced flap oscillation, 遷音速風洞, alternating direction implicit形式, 超音速輸送機, aeroelastic response, computational fluid dynamics, ADI form, total variation diminishing, SST, alternating direction implicit form, 数値シミュレーション, 全変動減少, フラップ強制振動, numerical simulation, 薄層ナビエ・ストークス方程式, 空力弾性応答, CFD, TVD

URL الوصول: https://explore.openaire.eu/search/publication?articleId=jairo_______::c06d534e105f00cff935602c02e32d40
http://id.nii.ac.jp/1696/00037314/