基于频响函数识别直升机尾传动轴系非线性的方法
单卫东1，臧朝平1，张根辈1，王平2，邹亚晨2，倪徳2
Method for identifying the nonlinearity of a helicopter tail drive shaft system based on frequency response functions
SHAN Weidong1，ZANG Chaoping1，ZHANG Genbei1，WANG Ping2，ZOU Yachen2，NI De2
振动与冲击
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2020, (14): 102
-108
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