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超音速機概念設計ツールCAPASの開発
https://jaxa.repo.nii.ac.jp/records/5423
https://jaxa.repo.nii.ac.jp/records/54232df104b3-6fad-4c8c-87d2-24cf407b4367
名前 / ファイル | ライセンス | アクション |
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64303021.pdf (1.7 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 | 超音速機概念設計ツールCAPASの開発 | |||||
言語 | ||||||
言語 | jpn | |||||
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 | Development of CAPAS, conceptual design tool for supersonic aircraft | |||||
著者 |
牧野, 好和
× 牧野, 好和× 牧本, 卓也× Makino, Yoshikazu× Makimoto, Takuya |
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著者所属 | ||||||
宇宙航空研究開発機構 | ||||||
著者所属 | ||||||
菱友システムズ | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Ryoyu Systems | ||||||
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: 第40回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2008論文集 en : JAXA Special Publication: Proceedings fo 40th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2008 巻 JAXA-SP-08-009, 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 | 第40回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2008. 会期: 2008年6月12日-6月13日. 会場: 東北大学片平キャンパス | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A new design system called CAPAS (CAD-based Automatic Panel Analysis System) has been developed for design automation in the S-cube (Silent SuperSonic) program at JAXA. CAPAS has a java-based GUI (Graphical User Interface) for designers to use it easily and effectively. The system comprises 4 design processes; geometry definition of airplane components, airplane CAD model generation, aerodynamic analysis, and sonic-boom analysis. The geometries of some airplane components defined by a designer are combined in a full airplane configuration automatically by CAD-based program that utilizes the geometry definition API (Application Programming Interface) of CATIA(R) V4/V5. The A502 Panair analysis is executed in this system after setting the analysis parameters such as Mach number or angles of attacks. The near-field pressure signatures calculated by A502 analysis as well as force data is extrapolated to the ground by the Thomas code based on a modified linear theory to estimate the sonic-boom. | |||||
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: AA0064303021 | |||||
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-08-009 |