A Mathematical Model for Dynamic Vibration Analysis of a Landing Aircraft

被引:0
|
作者
Guo-guang Liu
Lei-yang Pei
Li Feng
Zhi-wei Wu
机构
[1] Civil Aviation University of China,College of Transportation Science and Engineering
[2] Sun Yat-Sen University,School of Civil Engineering
[3] Hangke Technology Development Co.,undefined
[4] Ltd,undefined
关键词
Aircraft vibration; Runway pavement; Wing up-lift effect; The third-aircraft vibration model; Power spectral density (PSD); Mechanical performance optimization;
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中图分类号
学科分类号
摘要
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页码:4149 / 4162
页数:13
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