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某型飞机高原起降前轮摆振特性分析
引用本文:曾德军,吴建刚,李曙林,王鹏,姜磊.某型飞机高原起降前轮摆振特性分析[J].沈阳航空工业学院学报,2005,22(2):7-9.
作者姓名:曾德军  吴建刚  李曙林  王鹏  姜磊
作者单位:空军工程大学工程学院,陕西,西安,710038
摘    要:前轮摆振是飞机结构动力学的主要研究课题之一,文章应用前轮摆振理论,结合高原机场的使用特点,分析了某型飞机在高原环境下起降的前轮摆振特性,得出该型飞机高原起降的摆振特性曲线。并与该型飞机的平原摆振特性进行了对比分析。

关 键 词:摆振  前轮  高原  临界阻尼
文章编号:1007-1385(2005)02-0007-03
修稿时间:2004年11月3日

Nose wheel vibration character analysis of certain aircraft taking off and landing in plateau area
ZENG De-jun,WU Jian-gang,LI Shu-lin,WANG Peng,JIANG Lei.Nose wheel vibration character analysis of certain aircraft taking off and landing in plateau area[J].Journal of Shenyang Institute of Aeronautical Engineering,2005,22(2):7-9.
Authors:ZENG De-jun  WU Jian-gang  LI Shu-lin  WANG Peng  JIANG Lei
Abstract:The vibration character of nose wheel is one of the major topics of aircraft structural dynamics.Based on the theory of vibration and combines with characteristic in use,the paper analyzed the dynamic characteristics of nose wheel in plateau environment for certain type aircraft, and the curve of the vibration characteristics of nose wheel was given out.Excepting this,the contrasting analysis with plain area character was made.
Keywords:vibration  nose wheel  plateau  critical damp  
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