大迎角机动进气道装置刚柔耦合动力学分析
Developing the inlet test installation for with high AOA maneuver the inlet’s characteristics of aircraft in the flight is studied.According to structural features and the motion mode,combining with the theory of flexible,and based on the modal synthesis method,the rigid and flexible coupling model...
Saved in:
| Main Authors: | 孔鹏, 王克逸, 巫朝君 |
|---|---|
| Format: | Article |
| Language: | zho |
| Published: |
Editorial Office of Journal of Mechanical Transmission
2012-01-01
|
| Series: | Jixie chuandong |
| Online Access: | http://www.jxcd.net.cn/thesisDetails#10.16578/j.issn.1004.2539.2012.08.032 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
齿轮系统刚柔耦合动力学建模与仿真研究
by: 王炎, et al.
Published: (2009-01-01) -
采煤机截割部的刚柔耦合动力学分析
by: 赵丽娟, et al.
Published: (2011-01-01) -
基于刚柔耦合建模的平行分度凸轮机构动力学分析
by: 赵浩东, et al.
Published: (2011-01-01) -
刚—弹耦合齿轮多体动力学模型研究
by: 黄祝庆, et al.
Published: (2012-01-01) -
平面双曲柄冲压机刚柔耦合模型的动态仿真
by: 刘波, et al.
Published: (2012-01-01)