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静粛超音速研究機の空力設計の概要
https://jaxa.repo.nii.ac.jp/records/5449
https://jaxa.repo.nii.ac.jp/records/5449381ffadc-adc4-43aa-a0ef-c086bee8cb4f
名前 / ファイル | ライセンス | アクション |
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64239013.pdf (6.9 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 | ||||||
タイトル | 静粛超音速研究機の空力設計の概要 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Aerodynamic Design, Optimization, Supersonic Transport, Sonic-Boom | |||||
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 | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Introduction of aerodynamic design of a silent supersonic technology demonstrator | |||||
著者 |
牧野, 好和
× 牧野, 好和× Makino, Yoshikazu |
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著者所属 | ||||||
宇宙航空研究開発機構航空プログラムグループ超音速機チーム | ||||||
著者所属(英) | ||||||
en | ||||||
Aviation Program Group, Japan Aerospace Exploration Agency (JAXA) | ||||||
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: 小型超音速実験機(ロケット実験機)飛行実験データ解析完了報告 en : JAXA Special Publication 巻 JAXA-SP-08-008, 発行日 2009-02-27 |
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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 | 小型超音速実験機(ロケット実験機)飛行実験データ解析完了報告会(平成20年7月10日. 東京大学山上会館) | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | JAXA's planned scaled low-boom demonstrator project and its aerodynamic design in conceptual design phase are introduced. For the demonstration of low sonic-boom design concepts and design technology, this demonstrator named Silent SuperSonic Technology Demonstrator (S3TD) is designed using JAXA's computer-based aerodynamic design tools for low-drag and low-boom configuration. A multidisciplinary design exploration, in which the aerodynamic performance estimated by an unstructured Euler CFD code, sonic-boom intensity, and structural constraints are taken into account, is applied to the design of the demonstrator as well as an aerodynamic conceptual design tool based on a low-fidelity panel method. Several design cycles are conducted through the validation process for mission requirement with many CFD analyses and wind-tunnel tests. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
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: AA0064239013 | |||||
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-08-008 |