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Progress in aerodynamic technology to support a second-generation supersonic transport
https://jaxa.repo.nii.ac.jp/records/5754
https://jaxa.repo.nii.ac.jp/records/575412ec4525-00ee-42a0-8672-3ac63aee4ffa
名前 / ファイル | ライセンス | アクション |
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63609023.pdf (6.3 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Progress in aerodynamic technology to support a second-generation supersonic transport | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 超音速機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 航空機設計 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 民間航空 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 計算流体力学 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 旅客機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 翼型設計 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 設計最適化 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 翼平面形 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 揚抗比 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 翼型 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 抗力低減 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ヨーロッパ | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | supersonic aircraft | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aircraft design | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | civil aviation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | computational fluid dynamics | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | passenger aircraft | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wing design | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | design optimization | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wing planform | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | lift drag ratio | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | airfoil | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | drag reduction | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Europe | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
著者 |
Lovell, D. A.
× Lovell, D. A. |
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著者所属 | ||||||
Defence Evaluation and Research Agency Applied Aerodynamics | ||||||
著者所属(英) | ||||||
en | ||||||
Defence Evaluation and Research Agency Applied Aerodynamics | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構 | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構特別資料 en : JAXA Special Publication: Proceedings of International Workshops on Numerical Simulation Technology for Design of Next Generation Supersonic Civil Transport (SST-CFD Workshop) 巻 JAXA-SP-06-029E, p. 204-216, 発行日 2007-03-30 |
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会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | SST-CFDワークショップ.次世代超音速機の数値シミュレーション利用技術に関する国際ワークショップ 航空宇宙技術研究所 20000117-20000119 東京 日本 | |||||
会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | SST-CFD Workshop. International Workshops on Numerical Simulation Technology for Design of Next Generation Supersonic Civil Transport National Aerospace Laboratory 20000117-20000119 Tokyo Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The paper describes some aspects of the development and application within UK and mainland Europe of the aerodynamic technology required for successful design by industry of the next generation of supersonic transport aircraft. The focus is on wing design, but the methods covered are equally applicable to the design of other components and their interaction. Three areas are covered. Firstly a design method for aerodynamic shapes, developed at DERA (Defense Evaluation and Research Agency) UK, is summarized and two applications are described: an investigation of dual-point transonic/supersonic aerofoil design using an Euler CFD (Computational Fluid Dynamics) code, and the dual-point design of a delta-wing/body combination using a multi-block Euler CFD code. Secondly the initial application of the wing shape optimization method to the dual-point design of a supersonic transport wing is summarized. Finally results from a European research project on the reduction of drag and the assessment of aerodynamic design methods are presented. Two linked wing-design tasks were completed: dual-point transonic/supersonic cruise design and low-speed high-lift design. Three wing configurations were tested at low-speed, transonically and supersonically. Figures showing a selection of the measured forces and pressures indicate the effectiveness of the aerodynamic design. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-113X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11984031 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063609023 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-SP-06-029E |