Aerodynamic Effects of Asymmetric Pitching of Biplane Flapping Wing Micro Air Vehicle
文献类型：会议论文
| 作者 | Cui L(崔龙) ; Wang HW(王洪伟); Jiang T(江涛); Tian, Shen
|
| 出版日期 | 2017 |
| 会议名称 | The 9th Asian-Pacific Conference on Aerospace Technology and Science & The 2nd Asian Joint Symposium on Aerospace |
| 会议日期 | November 20-23, 2017 |
| 会议地点 | Beijing, China |
| 关键词 | flapping wing biplane asymmetric pitching aerodynamics |
| 页码 | 349-349 |
| 通讯作者 | Cui L(崔龙) |
| 中文摘要 | The aerodynamics of flapping wing micro air vehicle (FMAV) are significantly affected by the wing kinematics, of which are mainly flapping and pitching of the wings. And the design of wing kinematics pattern is an effective way to modulate the lift and thrust, consequently the control the vehicle. Here, such pattern of wing motion for hovering flapping flight is studied using computational fluid dynamics (CFD). This work is highlighted by the insights into asymmetric pitching and the effects of it on the aerodynamic performance. It is found that the thrust benefits from this wing kinematics configuration and the lift is also greatly influenced by this. Explanation of these phenomenon are discussed. And other important factors relating to the design of a practical FMAV are also noted. |
| 产权排序 | 1 |
| 会议录 | Proceedings of 2017 Asian-Pacific Conference on Aerospace Technology and Science & The 2nd Asian Joint Symposium on Aerospace Engineering
 |
| 语种 | 英语 |
| 源URL | [http://ir.sia.cn/handle/173321/21341]  |
| 专题 | 沈阳自动化研究所_机器人学研究室 |
| 作者单位 | Shenyang institute of Automation Chinese Academy of Sciences, Shenyang China |
| 推荐引用方式 GB/T 7714 | Cui L,Wang HW,Jiang T,et al. Aerodynamic Effects of Asymmetric Pitching of Biplane Flapping Wing Micro Air Vehicle[C]. 见:The 9th Asian-Pacific Conference on Aerospace Technology and Science & The 2nd Asian Joint Symposium on Aerospace. Beijing, China. November 20-23, 2017. |
入库方式： OAI收割
来源：沈阳自动化研究所
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