Design and aerodynamic simulation of low Reynolds number rotor airfoil | |
Gao, Q.-J.; Y. Bai; Q. Sun; Z. Zhao; C.-J. Zhao and X. Gong | |
刊名 | Guangxue Jingmi Gongcheng/Optics and Precision Engineering
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2015 | |
卷号 | 23期号:2页码:511-519 |
英文摘要 | This research focuses on the thin circular arc rotor airfoils at a low Reynolds number. A novel thin circular arc airfoil with a convex structure was designed in consideration of its demand for high aerodynamic performance, high structural strength, lightweighting and easy manufacture. A convex curve on the upper surface of the airfoil was adopted to increase the thickness of airfoil at the partial chord and a stiffener in the airfoil was installed to improve the structural strength of blade span wise. The designed thin circular arc airfoil has the maximum thickness of 4.3%, a circular average thickness of 2.5%, the maximum camber of 5.5% and an average camber of 4.5%. Numerical simulations for computing the aerodynamic performance of the airfoil were performed at the representative Reynolds number between 40,000 and 100,000, and the angle of attack (AOA) from-4to 12 by using the two dimensional steady and incompressible Navier-Stoke equations. The pressure coefficient distribution line of airfoil surfaces and the velocity vector were acquired. A carbon fiber rotor with a diameter of 40 cm, a mass of 15 g and rotor pitch of 15.7 cm was manufactured with the present airfoil, and the experiments on the lift force and the structural strength in a hover state were performed and the results show the performance of the airfoil meets the use requirments. At present, the developed rotor airfoil has been successfully used in a rotor aircraft. , 2015, Chinese Academy of Sciences. All right reserved. |
收录类别 | EI |
内容类型 | 期刊论文 |
源URL | [http://ir.ciomp.ac.cn/handle/181722/56029] ![]() |
专题 | 长春光学精密机械与物理研究所_中科院长春光机所知识产出 |
推荐引用方式 GB/T 7714 | Gao, Q.-J.,Y. Bai,Q. Sun,et al. Design and aerodynamic simulation of low Reynolds number rotor airfoil[J]. Guangxue Jingmi Gongcheng/Optics and Precision Engineering,2015,23(2):511-519. |
APA | Gao, Q.-J.,Y. Bai,Q. Sun,Z. Zhao,&C.-J. Zhao and X. Gong.(2015).Design and aerodynamic simulation of low Reynolds number rotor airfoil.Guangxue Jingmi Gongcheng/Optics and Precision Engineering,23(2),511-519. |
MLA | Gao, Q.-J.,et al."Design and aerodynamic simulation of low Reynolds number rotor airfoil".Guangxue Jingmi Gongcheng/Optics and Precision Engineering 23.2(2015):511-519. |
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