4.7 Article

Visualization of hidden delamination and debonding in composites through noncontact laser ultrasonic scanning

Journal

COMPOSITES SCIENCE AND TECHNOLOGY
Volume 100, Issue -, Pages 10-18

Publisher

ELSEVIER SCI LTD
DOI: 10.1016/j.compscitech.2014.05.029

Keywords

Non-destructive testing; Ultrasonics; Debonding; Delamination; Laser ultrasonic imaging

Funding

  1. Korea Institute of Energy Technology Evaluation and Planning (KETEP) - Korea government Ministry of Trade, Industry and Energy [20123030020010]
  2. National Research Foundation (NRF) - Ministry of Science, ICT and Future Planning [2010-0017456]
  3. Southeast University [3250254202]
  4. Korea Evaluation Institute of Industrial Technology (KEIT) [20123030020010] Funding Source: Korea Institute of Science & Technology Information (KISTI), National Science & Technology Information Service (NTIS)

Ask authors/readers for more resources

This study proposes a complete noncontact laser ultrasonic wavefield imaging technique to automatically detect and visualize hidden delamination and debonding in composite structures. First, ultrasonic wavefield is obtained from a target structure by scanning a Nd:YAG pulse laser beam for ultrasonic wave generation and measuring the corresponding ultrasonic responses using a laser Doppler vibrometer. Then, hidden damages are identified and visualized through adoption of a standing wave filter, which can isolate damage-induced standing waves from the obtained wavefield. The proposed technique has following advantages over the existing techniques: (1) it does not require any sensor installation; (2) it is noninvasive, rapidly deployable and applicable to harsh environments; and (3) it can visualize damage with high spatial resolution without any baseline data, which enables automated and intuitive damage diagnosis. The feasibility of the proposed technique is demonstrated by visualizing a debonding in a carbon fiber reinforced plastic aircraft wing and a delamination in a glass fiber reinforced plastic wind turbine blade. Furthermore, the effects of temperature and static loading variations on the proposed technique are also examined. (C) 2014 Elsevier Ltd. All rights reserved.

Authors

I am an author on this paper
Click your name to claim this paper and add it to your profile.

Reviews

Primary Rating

4.7
Not enough ratings

Secondary Ratings

Novelty
-
Significance
-
Scientific rigor
-
Rate this paper

Recommended

No Data Available
No Data Available