Wind tunnel test for drag reduction of airfoil bionic soft surface

CORC > 长春光学精密机械与物理研究所 > 中国科学院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 > 会议论文

	Wind tunnel test for drag reduction of airfoil bionic soft surface
	Zhang X.-P. ; Wang Y.-H. ; Ren L.-Q.
	2014
会议名称	4th International Conference of Bionic Engineering, ICBE 2013, August 13, 2013 - August 16, 2013
会议地点	Nanjing, China
页码	767-778
英文摘要	The soft surface of birds and aquatic organisms in the nature can effectively reduce the drag. Inspired by the fact in this paper, an attempt is made to stick silicone rubber soft surface on the surfaces of NACA 4412 and NACA 6409 airfoils. The drags, lifts and lift-drag ratios of airfoils with soft and rigid surfaces in 5 different thickness were compared through wind tunnel test under the condition of = 0 . The results show that most of the bionic soft surfaces play the role of reducing the aerodynamic drag, and also increasing the lift at the same time, in which the soft surface of 0.6mm had the most significant effect of drag reduction and lift increasing. (2014) Trans Tech Publications, Switzerland.
收录类别	EI
会议录	4th International Conference of Bionic Engineering, ICBE 2013, August 13, 2013 - August 16, 2013
会议录出版者	Trans Tech Publications Ltd
会议录出版地	Nanjing, China
语种	英语
内容类型	会议论文
源URL	[http://ir.ciomp.ac.cn/handle/181722/44569]
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_会议论文
推荐引用方式 GB/T 7714	Zhang X.-P.,Wang Y.-H.,Ren L.-Q.. Wind tunnel test for drag reduction of airfoil bionic soft surface[C]. 见:4th International Conference of Bionic Engineering, ICBE 2013, August 13, 2013 - August 16, 2013. Nanjing, China.