A Simplified Flexible Multibody Dynamics for a Main Landing Gear with Flexible Leaf Spring
Xue Z. P. ; Li M. ; Li Y. H. ; Jia H. G.
刊名Shock and Vibration
2014
卷号10
ISSN号ISBN/1070-9622
英文摘要The dynamics of multibody systems with deformable components has been a subject of interest in many different fields such as machine design and aerospace. Traditional rigid-flexible systems often take a lot of computer resources to get accurate results. Accuracy and efficiency of computation have been the focus of this research in satisfying the coupling of rigid body and flex body. The method is based on modal analysis and linear theory of elastodynamics: reduced modal datum was used to describe the elastic deformation which was a linear approximate of the flexible part. Then rigid-flexible multibody system was built and the highly nonlinearity of the mass matrix caused by the limited rotation of the deformation part was approximated using the linear theory of elastodynamics. The above methods were used to establish the drop system of the leaf spring type landing gear of a small UAV. Comparisons of the drop test and simulation were applied. Results show that the errors caused by the linear approximation are acceptable, and the simulation process is fast and stable.
收录类别SCI
语种英语
内容类型期刊论文
源URL[http://ir.ciomp.ac.cn/handle/181722/43700]  
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
Xue Z. P.,Li M.,Li Y. H.,et al. A Simplified Flexible Multibody Dynamics for a Main Landing Gear with Flexible Leaf Spring[J]. Shock and Vibration,2014,10.
APA Xue Z. P.,Li M.,Li Y. H.,&Jia H. G..(2014).A Simplified Flexible Multibody Dynamics for a Main Landing Gear with Flexible Leaf Spring.Shock and Vibration,10.
MLA Xue Z. P.,et al."A Simplified Flexible Multibody Dynamics for a Main Landing Gear with Flexible Leaf Spring".Shock and Vibration 10(2014).
个性服务
查看访问统计
相关权益政策
暂无数据
收藏/分享
所有评论 (0)
暂无评论
 

除非特别说明,本系统中所有内容都受版权保护,并保留所有权利。


©版权所有 ©2017 CSpace - Powered by CSpace