Torsional guided wave-based debonding detection in honeycomb sandwich beams

被引:11
|
作者
Zhu, Kaige [1 ,2 ]
Qing, Xinlin P. [3 ]
Liu, Bin [2 ]
机构
[1] COMAC, Beijing Aeronaut Sci & Technol Res Inst, Beijing 102211, Peoples R China
[2] Tsinghua Univ, Sch Aerosp, AML, Beijing 100084, Peoples R China
[3] Xiamen Univ, Sch Aerosp Engn, Xiamen 361005, Peoples R China
基金
中国博士后科学基金; 中国国家自然科学基金;
关键词
debonding detection; torsional guided wave; honeycomb sandwich; finite element method; non-destructive evaluation; LAMB WAVE; NONDESTRUCTIVE EVALUATION; COMPOSITE STRUCTURES; TIME-REVERSAL; DAMAGE; INSPECTION; IDENTIFICATION; PROPAGATION; FREQUENCY; LINE;
D O I
10.1088/0964-1726/25/11/115048
中图分类号
TH7 [仪器、仪表];
学科分类号
0804 ; 080401 ; 081102 ;
摘要
Debonding is one of the most dangerous damages in honeycomb sandwich structures, which causes stiffness reduction and is invisible from the surface. Guided wave-based non-destructive evaluation is a promising approach with high sensitivity and high efficiency for debonding detection. A torsional guided wave method is proposed to inspect debonding damage in honeycomb sandwich beams, which is proved to be better in damage location for the beams in the paper than the flexural wave used before. The honeycomb heterogeneity effect on the interaction between guided waves and debonding are first investigated by finite element methods. Then the ability of torsional waves to determine debonding locations and sizes is discussed in detail. Finally, in order to verify the proposed method, experiments are carried out to inspect debonding damage with two sizes.
引用
收藏
页数:11
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