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ロータ間の空力干渉における位相角差の影響に対する考察
https://jaxa.repo.nii.ac.jp/records/3240
https://jaxa.repo.nii.ac.jp/records/324053bea8de-ba26-419e-b445-9cd6301f5d09
名前 / ファイル | ライセンス | アクション |
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AA1730011006.pdf (2.7 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2017-12-28 | |||||
タイトル | ||||||
タイトル | ロータ間の空力干渉における位相角差の影響に対する考察 | |||||
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 of Influence of Phase-angle Differences on Aerodynamic Interactions between Rotors | |||||
著者 |
田中, 陸久
× 田中, 陸久× 田辺, 安忠× 砂田, 茂× 米澤, 宏一× 得竹, 浩× 新井, 隆景× Tanaka, Riku× Tanabe, Yasutada× Sunada, Shigeru× Yonezawa, Koichi× Tokutake, Hiroshi× Arai, Takakage |
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著者所属 | ||||||
大阪府立大学 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
名古屋大学 | ||||||
著者所属 | ||||||
電力中央研究所 (CRIEPI) | ||||||
著者所属 | ||||||
金沢大学 | ||||||
著者所属 | ||||||
大阪府立大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Osaka Prefecture University | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Nagoya University | ||||||
著者所属(英) | ||||||
en | ||||||
Central Research Institute of Electric Power Industry (CRIEPI) | ||||||
著者所属(英) | ||||||
en | ||||||
Kanazawa University | ||||||
著者所属(英) | ||||||
en | ||||||
Osaka Prefecture University | ||||||
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49回流体力学講演会/第35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 49th Fluid Dynamics Conference / the 35th Aerospace Numerical Simulation Symposium 巻 JAXA-SP-17-004, p. 53-59, 発行日 2017-12-27 |
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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49回流体力学講演会/第35回航空宇宙数値シミュレーション技術シンポジウム (2017年6月28日-36日. 国際オリンピック記念青少年総合センター), 渋谷区, 東京 | |||||
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 | 49th Fluid Dynamics Conference /the 35th Aerospace Numerical Simulation Symposium (June 28-30, 2017. National Olympics Memorial Youth Center), Shibuya-ku, Tokyo, Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Aerodynamic interactions between 6 rotors on a multi-copter type drone are numerically simulated. The phase angles of the rotors and the pitch angles of the rotor blades are varied. The total thrust changes about 3% due to phase angle differences. With the phase angle differences between the neighboring rotors fixed to the smallest angle about 0 degrees (Worstcase), as the pitch angle approaches 16deg, the oscillating forces become relatively low. This property of the oscillating forces depends on the phase angle differences between the rotors, which is considered to be due to the shape change of the tip vortices. | |||||
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: AA1730011006 | |||||
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-17-004 |