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4枚ブレード・ロータを用いたBVI騒音計測基礎試験
https://jaxa.repo.nii.ac.jp/records/38189
https://jaxa.repo.nii.ac.jp/records/381896e9273e9-15d0-42ab-bd52-5109909e8291
名前 / ファイル | ライセンス | アクション |
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nalsp0055209.pdf (111.7 kB)
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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 | 4枚ブレード・ロータを用いたBVI騒音計測基礎試験 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 騒音測定 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | BVI | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | CFD | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 4枚ブレード・ロータ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 圧力センサ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風速 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 翼 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 低速風洞 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | マイクロフォン | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 研究開発 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 音響波形 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ヘリコプター | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | noise measurement | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | BVI | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | CFD | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | 4-bladed model rotor | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | pressure sensor | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind velocity | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wing | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | low speed wind tunnel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | microphone | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | research and development | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | acoustic waveform | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | helicopter | |||||
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 | BVI noise measurement using 4-bladed model rotor in NAL | |||||
著者 |
近藤, 夏樹
× 近藤, 夏樹× 末永, 尚史× 白井, 正孝× 齊藤, 茂× 足立, 直人× 前田, 一郎× 中尾, 雅弘× Kondo, Natsuki× Suenaga, Hisashi× Shirai, Masataka× Saito, Shigeru× Adachi, Naoto× Maeda, Ichiro× Nakao, Masahiro |
|||||
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 | ||||||
航空宇宙技術研究所 | ||||||
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(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
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 | ||||||
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. | ||||||
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: 平成14年度航空安全・環境適合技術研究研究交流会と研究報告会講演論文集 en : Special Publication of National Aerospace Laboratory: Proceedings of the Information Exchange Meeting and the Research Meeting on Aviation Safety and Environmental Compatibility Technology Research FY2001 巻 55, p. 89-92, 発行日 2002-12 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This paper presents measured blade vortex interaction (BVI) noise using the 4-bladed model rotor in NAL. The tested blades have a rectangular tip and a twisted NACA0012 profile. Pressure history in the tip region on the blade surface was measured using pressure transducers. Acoustic waveform was measured using three fixed microphones. Two of them were located at 2.25 R away from the rotor center on the advancing and retreating sides, respectively. The other was located below the rotor plane on the advancing side. As a result, the strongest BVI noise was measured in the case of advance ratio of 0.16, shaft tilt angle of 4 deg, and thrust coefficient of 0.0080. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1347-457X | |||||
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: AA0045946009 | |||||
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-55 |