JAXA Repository / AIREX 未来へ続く、宙(そら)への英知
titleマルチコプタのロータ間の空力干渉
Other TitleAerodynamic Interactions Between Rotors on a Multi-Copter Drone
Author(jpn)田辺, 安忠; 青山, 剛史; 杉浦, 正彦; 菅原, 瑛明; 砂田, 茂; 米澤, 宏一; 得竹, 浩
Author(eng)Tanabe, Yasutada; Aoyama, Takashi; Sugiura, Masahiko; Sugawara, Hideaki; Sunada, Shigeru; Yonezawa, Koichi; Tokutake, Hiroshi
Author Affiliation(jpn)宇宙航空研究開発機構(JAXA); 宇宙航空研究開発機構(JAXA); 宇宙航空研究開発機構(JAXA); 株式会社菱友システムズ; 大阪府立大学; 大阪大学; 金沢大学
Author Affiliation(eng)Japan Aerospace Exploration Agency (JAXA); Japan Aerospace Exploration Agency (JAXA); Japan Aerospace Exploration Agency (JAXA); Ryoyu Systems Co., Ltd.; Osaka Prefecture University; Osaka University; Kanazawa University
Issue Date2016-12-27
Publisher宇宙航空研究開発機構(JAXA)
Japan Aerospace Exploration Agency (JAXA)
Publication title宇宙航空研究開発機構特別資料: 第48回流体力学講演会/第34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
JAXA Special Publication: Proceedings of the 48th Fluid Dynamics Conference / the 34th Aerospace Numerical Simulation Symposium
VolumeJAXA-SP-16-007
Start page141
End page146
Publication date2016-12-27
Languagejpn
eng
AbstractAerodynamic interactions between 6 rotors on a multi-copter type drone are numerically simulated. The pitch angle of the rotor blades and the distance between the rotors are varied. It is found that 2-6/rev fluctuations in the resultant forces and moments are significant due to the interactions between these 6 rotors. These oscillating forces and moments are considered to be the main sources of vibrations on the multi-copter type drone. The thrust of the drone is controlled by change of the rotor pitch and the fluctuations change in nearly same proportion with the resultant thrust. When the distance between the rotor is below half of the rotor radius, the intensity of the interaction increases abruptly to about 3 times while the rotor performance improves about 20% compared with the wide rotor distance cases.
Description会議情報: 第48回流体力学講演会/第34回航空宇宙数値シミュレーション技術シンポジウム (2016年7月6日-8日. 金沢歌劇座), 金沢市, 石川
形態: カラー図版あり
Meeting Information: 48th Fluid Dynamics Conference /the 34th Aerospace Numerical Simulation Symposium (July 6-8, 2016. The Kanazawa Theatre), Kanazawa, Ishikawa, Japan
Physical characteristics: Original contains color illustrations
Document TypeConference Paper
JAXA Category特別資料
NASA Subject CategoryAircraft Design, Testing and Performance
ISSN1349-113X
NCIDAA11984031
SHI-NOAA1630031017
Report NoJAXA-SP-16-007
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/577441


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