Gust Alleviation Device Applied to the Sensorcraft Structure

摘要：

A gust alleviation model is presented and its effectiveness will be demonstrated on the sensorcraft structure. A simple rectangular wing will be used to perform a parametric study in order to study the effect of the different parameters, such as stiffness attachment, sweep, size of gust device, etc. Consideration is made of the feasibility of incorporating an adaptive torsional stiffness attachment that could be used to trim the device for more efficient flight, and also to enable roll control.

关键词： Gust alleviation aeroelasticity active structures sensorcraft

作者: Gareth A. Vio Simon Miller Jonathan E. Cooper

作者单位: School of Aerospace, Mechanical and Mechatronic Engineering, University of Sydney,Sydney NSW 2006, A School of Engineering, University of Manchester, Manchester M13 9PL, UK Department of Engineering, University of Liverpool, Brownlow Hill, Liverpool L69 7ZF, UK

会议类型: 国际会议

会议名称: 2011年亚太航空航天技术学术会议(APISAT 2011)

会议地点: 澳大利亚

会议语种:英文

页码: 1-11

在线出版日期: 2011-02-28（万方平台首次上网日期，不代表论文的发表时间）