Theoretical analysis and experimental verification of nonlinear vibrational response of cracked blade

被引：0
|
作者：
裂纹叶片非线性振动响应理论分析与实验验证
机构：
[1] [1,Shen, Guoji
[2] 1,Guan, Fengjiao
[3] 1,Bian, Zifang
[4] 1,Hu, Haifeng
[5] 1,Yang, Yongmin
来源：
Yang, Yongmin (yangyongmin@163.com); Yang, Yongmin (yangyongmin@163.com) | 2021年 / National University of Defense Technology卷 / 43期
关键词：
Analysis verification - Aviation safety - Blade - Cracked blade - Experimental verification - Non-linear vibrations - Nonlinearity - Power - Vibration - Vibrational response;
D O I：
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学科分类号：
摘要：
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页码：127 / 134
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