Simplified modeling method of impact damage for numerical simulation of Lamb wave propagation in quasi-isotropic composite structures

2020 ◽  
Vol 243 ◽  
pp. 112150 ◽  
Author(s):  
Peiwen Deng ◽  
Osamu Saito ◽  
Yoji Okabe ◽  
Hideki Soejima
2006 ◽  
Vol 75 (1-4) ◽  
pp. 267-275 ◽  
Author(s):  
Chunhui Yang ◽  
Lin Ye ◽  
Zhongqing Su ◽  
Michael Bannister

2016 ◽  
Vol 167 ◽  
pp. 109-115 ◽  
Author(s):  
A. De Luca ◽  
Z. Sharif-Khodaei ◽  
M.H. Aliabadi ◽  
F. Caputo

2013 ◽  
Vol 97 ◽  
pp. 387-400 ◽  
Author(s):  
Seyed Mohammad Hossein Hosseini ◽  
Abdolreza Kharaghani ◽  
Christoph Kirsch ◽  
Ulrich Gabbert

Author(s):  
Bo Zhang ◽  
Fang Liu ◽  
Chang Liu ◽  
Jingming Li ◽  
Baojun Zhang ◽  
...  

2018 ◽  
Vol 9 (1) ◽  
pp. 46 ◽  
Author(s):  
Nobuyuki Toyama ◽  
Jiaxing Ye ◽  
Wataru Kokuyama ◽  
Shigeki Yashiro

This study demonstrates a rapid non-contact ultrasonic inspection technique by visualization of Lamb wave propagation for detecting impact damage in carbon fiber reinforced polymer (CFRP) laminates. We have developed an optimized laser ultrasonic imaging system, which consists of a rapid pulsed laser scanning unit for ultrasonic generation and a laser Doppler vibrometer (LDV) unit for ultrasonic reception. CFRP laminates were subjected to low-velocity impact to introduce barely visible impact damage. In order to improve the signal-to-noise ratio of the detected ultrasonic signal, retroreflective tape and a signal averaging process were used. We thus successfully visualized the propagation of the pulsed Lamb A0 mode in the CFRP laminates without contact. Interactions between the Lamb waves and impact damage were clearly observed and the damage was easily detected through the change in wave propagation. Furthermore, we demonstrated that the damage could be rapidly detected without signal averaging. This method has significant advantages in detecting damage compared to the conventional method using a contact resonant ultrasonic transducer due to the absence of the ringing phenomenon when using the LDV.


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