会議発表論文 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

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

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.
会議情報: 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
形態: カラー図版あり
Meeting Information: 49th Fluid Dynamics Conference /the 35th Aerospace Numerical Simulation Symposium (June 28-30, 2017. National Olympics Memorial Youth Center), Shibuya-ku, Tokyo, Japan
Physical characteristics: Original contains color illustrations
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https://repository.exst.jaxa.jp/dspace/bitstream/a-is/865290/1/AA1730011006.pdf

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