WEKO3
アイテム
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翼後退角有無によるスラット騒音変化について
https://jaxa.repo.nii.ac.jp/records/2940
https://jaxa.repo.nii.ac.jp/records/294089af20f5-6dc3-4f25-8bca-7d70ccdea3d7
名前 / ファイル | ライセンス | アクション |
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AA1830029011.pdf (3.6 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2019-02-28 | |||||
タイトル | ||||||
タイトル | 翼後退角有無によるスラット騒音変化について | |||||
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 | Study on Influence of Wing Sweep Angle on the Slat Noise Characteristics | |||||
著者 |
村山, 光宏
× 村山, 光宏× 雨宮, 和久× 田中, 健太郎× 伊藤, 靖× 横川, 譲× 山本, 一臣× 池田, 友明× 平井, 亨× Murayama, Mitsuhiro× Amemiya, Kazuhisa× Tanaka, Kentaro× Ito, Yasushi× Yokokawa, Yuzuru× Yamamoto, Kazuomi× Ikeda, Tomoaki× Hirai, Toru |
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著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
株式会社エイ・エス・アイ総研 | ||||||
著者所属 | ||||||
株式会社菱友システムズ | ||||||
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 | ||||||
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 | ||||||
株式会社菱友システムズ | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Advanced Science & Intelligence Research Institute (ASIRI) | ||||||
著者所属(英) | ||||||
en | ||||||
Ryoyu Systems Co., Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Ryoyu Systems Co., Ltd. | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構(JAXA) | |||||
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50回流体力学講演会/第36回航空宇宙数値シミュレーション技術シンポジウム論文集 en : JAXA Special Publication: Proceedings of the 50th Fluid Dynamics Conference / the 36th Aerospace Numerical Simulation Symposium 巻 JAXA-SP-18-005, p. 121-126, 発行日 2019-02-25 |
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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50回流体力学講演会/第36回航空宇宙数値シミュレーション技術シンポジウム (2018年7月4日-6日. 宮崎市民プラザ), 宮崎市, 宮崎 | |||||
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 | 50th Fluid Dynamics Conference /the 36th Aerospace Numerical Simulation Symposium (July 4-6, 2018. Miyazaki Citizen's Plaza), Miyazaki, Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Aeroacoustic simulations associated with noise radiation from the leading-edge slat is conducted. The shear layer emanating from the slat cusp and its subsequent reattachment upstream of the slat trailing edge lead to a primarily broadband noise spectrum. Often, however, the slat noise spectrum also exhibits narrowband peaks superimposed on the broadband portion, especially in the case of unswept wind tunnel configurations at lower than full-scale Reynolds numbers. In this study, influence of wing sweep angle on the slat noise characteristics, especially on the narrowband peaks, is investigated by aeroacoustic simulation using Delayed Detached Eddy Simulation around the 30P30N three-element high-lift airfoil configuration. | |||||
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 | |||||
ISSNONLINE | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 2433-2232 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA1830029011 | |||||
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-18-005 |