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流路切り換え機構の空力解析
https://jaxa.repo.nii.ac.jp/records/36891
https://jaxa.repo.nii.ac.jp/records/36891b4cb5745-dfa3-4185-ad95-3980fa7c4044
名前 / ファイル | ライセンス | アクション |
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nalsp0034032.pdf (694.4 kB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 流路切り換え機構の空力解析 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 流路切替機構 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空力解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 可変バイパスファンエンジン | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | エンジン形態 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 比推力 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 超音速飛行 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 粘性解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 全圧損失 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | バイパス比 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 排気速度 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ナビエ・ストークス方程式 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 航空機計算空気力学 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flow switch device | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerodynamic analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | variable bypass fan engine | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | engine configuration | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | specific thrust | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | supersonic flight | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | viscous analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | total pressure loss | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | bypass ratio | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | jet velocity | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Navier Stokes equation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aircraft computational aerodynamics | |||||
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 | Aerodynamic analysis of the flow switch device | |||||
著者 |
清水, 邦弘
× 清水, 邦弘× 中西, 英全× 三宅, 慶明× 東森, 弘高× 野崎, 理× 菊地, 一雄× 田村, 敦宏× Shimizu, Kunihiro× Nakanishi, Hidemasa× Miyake, Yoshiaki× Higashimori, Hirotaka× Nozaki, Osamu× Kikuchi, Kazuo× Tamura, Atsuhiro |
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著者所属 | ||||||
三菱重工業 | ||||||
著者所属 | ||||||
三菱重工業 | ||||||
著者所属 | ||||||
三菱重工業 | ||||||
著者所属 | ||||||
三菱重工業 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Heavy Industries Ltd | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Heavy Industries Ltd | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Heavy Industries Ltd | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Heavy Industries Ltd | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory (NAL) | |||||
書誌情報 |
航空宇宙技術研究所特別資料 en : Special Publication of National Aerospace Laboratory 巻 34, p. 177-182, 発行日 1997-01 |
|||||
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 | 航空宇宙技術研究所 6-7 JUN. 1996 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 | National Aerospace Laboratory 6-7 JUN. 1996 Tokyo Japan | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 離着陸時の騒音を低減し、超音速飛行中の高比推力を得るエンジン形態として可変バイパスファンエンジンを提案した。流路切替え機構はバイパス比を変える一方法である。流路切替え機構の空力特性を把握するために、試験結果と比較しながら3次元粘性解析を行った。この解析は流路切替え機構の出口側における全圧損失を定性的に予測し、改良のための設計にかなり有効であることが分かった。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The variable bypass fan engine is proposed as an engine configuration to reduce noise at take-off & landing and to obtain high specific thrust during supersonic flight. The flow switch device is one of the methods to change bypass ratio. 3D viscous analysis was conducted to grasp the aerodynamic characteristics of the flow switch device, comparing with test results. The analysis qualitatively predicted the total pressure loss at the exit side of the flow switch device, and was proved to be quite useful for design improvement. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0289-260X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN10097345 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0000685032 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL SP-34 |