Experimental Validation of Improving Aircraft Rolling Power Using Piezoelectric Actuators

CORC > 力学研究所 > 中国科学院力学研究所 > 力学所知识产出(1956-2008)

	Experimental Validation of Improving Aircraft Rolling Power Using Piezoelectric Actuators
	Li M(李敏); Chen WM(陈伟民); Guan D(管德); Li W(李维)
刊名	Chinese Journal of Aeronautics
	2005
卷号	18 期号:2 页码:108-115
关键词	piezoelectric actuator rolling power wind tunnel experiment
ISSN号	1000-9361
其他题名	利用压电驱动器改善飞机横滚性能的试验验证
中文摘要	Piezoelectric actuators are mounted on both sides of a rectangular wing model. Possibility of the improvement of aircraft rolling power is investigated. All experiment projects, including designing the wind tunnel model, checking the material constants, measuring the natural frequencies and checking the effects of actuators, guarantee the correctness and precision of the finite element model. The wind tunnel experiment results show that the calculations coincide with the experiments. The feasibility of fictitious control surface is validated.
学科主题	力学
收录类别	EI ; CSCD
语种	英语
CSCD记录号	CSCD:2161170
公开日期	2007-06-15 ; 2007-12-05 ; 2009-06-23
内容类型	期刊论文
源URL	[http://dspace.imech.ac.cn/handle/311007/16321]
专题	力学研究所_力学所知识产出(1956-2008)
推荐引用方式 GB/T 7714	Li M,Chen WM,Guan D,et al. Experimental Validation of Improving Aircraft Rolling Power Using Piezoelectric Actuators[J]. Chinese Journal of Aeronautics,2005,18(2):108-115.
APA	李敏,陈伟民,管德,&李维.(2005).Experimental Validation of Improving Aircraft Rolling Power Using Piezoelectric Actuators.Chinese Journal of Aeronautics,18(2),108-115.
MLA	李敏,et al."Experimental Validation of Improving Aircraft Rolling Power Using Piezoelectric Actuators".Chinese Journal of Aeronautics 18.2(2005):108-115.