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超音速旅客機のエンジン配置に関する多分野統合最適設計
https://jaxa.repo.nii.ac.jp/records/22737
https://jaxa.repo.nii.ac.jp/records/22737a572c849-f0a9-4466-aedd-2222faa1fe80
Item type | 学術雑誌論文 / Journal Article(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2016-07-29 | |||||
タイトル | ||||||
タイトル | 超音速旅客機のエンジン配置に関する多分野統合最適設計 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Optimization | |||||
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 | Engine Integration | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||
資源タイプ | journal article | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Multidisciplinary Design Optimization of Engine Layout for Supersonic Airliner | |||||
著者 |
上野, 篤史
× 上野, 篤史× 渡辺, 安× Ueno, Atsushi× Watanabe, Yasushi |
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著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
出版者 | ||||||
出版者 | 日本航空宇宙学会 | |||||
出版者(英) | ||||||
出版者 | The Japan Society for Aeronautical and Space Sciences | |||||
書誌情報 |
航空宇宙技術 巻 14, p. 67-76, 発行日 2015-07-31 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The airframe/propulsion integration for supersonic airliners was studied considering three engine layouts (i.e., under-wing, over-wing, and side-body engines). In this study, the engine position was optimized for each layout from viewpoints of low-drag, low-boom, and high-range performances. This study revealed that the interference between nacelle shock wave and wing is important to achieve low-drag and low-boom, and that side-body engines realize the best compromise between them by setting engine so that the nacelle shock wave acts on the rear part of the wing. The engine position affects the inlet aerodynamic performance, which in turn affects the range performance. However, the side-body engine remains optimum, even when the range performance is taken into account. | |||||
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 | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1884-0477 | |||||
DOI | ||||||
識別子タイプ | DOI | |||||
関連識別子 | http://dx.doi.org/10.2322/astj.14.67 | |||||
関連名称 | info:doi/10.2322/astj.14.67 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: PA1620051000 |