Application of active structural health monitoring technique to aircraft fuselage structures

被引:27
|
作者
Castanien, KE [1 ]
Liang, C [1 ]
机构
[1] SAN DIEGO STATE UNIV,DEPT MECH ENGN,ACT CONTROL LAB,SAN DIEGO,CA 92182
关键词
NDE; structural health monitoring; electromechanical impedance analyzer; in-situ transducer array;
D O I
10.1117/12.239153
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
引用
收藏
页码:38 / 49
页数:12
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