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ロータ・アクティブ・コントロール基礎風洞試験
https://jaxa.repo.nii.ac.jp/records/38190
https://jaxa.repo.nii.ac.jp/records/38190117ba732-30e6-416f-9856-5054921c2c9e
名前 / ファイル | ライセンス | アクション |
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nalsp0055210.pdf (127.3 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 | ロータ・アクティブ・コントロール基礎風洞試験 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 風洞試験 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | アクティブ・フラップ制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 高調波制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 1枚ブレード・モデル・ロータ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | BVI | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 騒音低減 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ヘリコプター | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 音圧 | |||||
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 | CFD | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 位相制御 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | wind tunnel test | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | active flap control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | higher harmonic control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | single-blade model rotor | |||||
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 | noise reduction | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | helicopter | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | sound pressure | |||||
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 | CFD | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | phase control | |||||
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 | Elementary wind tunnel test of rotor active control | |||||
著者 |
近藤, 夏樹
× 近藤, 夏樹× 末永, 尚史× 白井, 正孝× 齊藤, 茂× 赤坂, 剛史× 田辺, 安忠× Kondo, Natsuki× Suenaga, Hisashi× Shirai, Masataka× Saito, Shigeru× Akasaka, Takeshi× Tanabe, Yasutada |
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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 | ||||||
川田工業 | ||||||
著者所属 | ||||||
川田工業 | ||||||
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 | ||||||
Kawada Industries Inc. | ||||||
著者所属(英) | ||||||
en | ||||||
Kawada Industries Inc. | ||||||
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. 93-96, 発行日 2002-12 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This paper shows the results of the elementary wind tunnel test of blade active control using a 1-bladed model rotor at the 2.5 m x 2.5 m multi-purpose wind tunnel in Kawada Industry. In this test, the effects of higher harmonic control (HHC) and active flap control (AFC) on rotor blade-vortex interaction (BVI) noise were investigated. The frequency of the control was 20 Hz (2/rev), and the amplitudes of HHC and AFC were +/- 2.0 deg and +/- 15.0 deg, respectively. The phase of control was changed at intervals of 45 deg. Two types of BVI were tested. The one is the parallel vortex interaction using the vortex generator upstream of a non-lifting rotor. The other is self-generated vortex interaction of a lifting rotor. As a result, the effects of BVI noise reduction were observed in the some cases. | |||||
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: AA0045946010 | |||||
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 |