首页 | 本学科首页   官方微博 | 高级检索  
     检索      

利用配重改善平尾颤振特性方法的研究
引用本文:刘济科,杨智春.利用配重改善平尾颤振特性方法的研究[J].强度与环境,1995(4):37-40.
作者姓名:刘济科  杨智春
作者单位:西北工业大学!西安,710072
摘    要:针对某型飞机平尾颤振速度偏低的实际问题,详细探讨了利用配重提高颤振速度的方案。分析方法及所得结果将有助于改善平尾的颤振特性,从而提高颤振速度。

关 键 词:航空器  颤振分析  配重  质量分布  水平尾翼

Research on measures to improve flutter properties of horizontal tail by use of attached weights
Liu Jike, Yang Zhichun, Zhao Lingcheng.Research on measures to improve flutter properties of horizontal tail by use of attached weights[J].Structure & Environment Engineering,1995(4):37-40.
Authors:Liu Jike  Yang Zhichun  Zhao Lingcheng
Abstract:It is a very important actual problem to be solved in aircraft engineering that the flutter speed of horizontal tail is lower than designed. To this end, by making use of attached weights, several measures are put forward to improve the flutter properties of horizontal tail of certain type aircraft. The analytical methods and the results obtained will be conductive to increase the flutter speed of horizontal tail.
Keywords:Flutter analysis  Counterbalances  Mass distribution  Vibration damping  Horizontal tail surface  
本文献已被 CNKI 维普 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号