Composite aircraft debonding visualization by laser ultrasonic scanning excitation and integrated piezoelectric sensing-Reference-Cited by-同舟云学术

Composite aircraft debonding visualization by laser ultrasonic scanning excitation and integrated piezoelectric sensing

Published:2012-06-08 Issue:7 Volume:19 Page:605-620
ISSN:1545-2255
Container-title:Structural Control and Health Monitoring
language:en
Short-container-title:Struct. Control Health Monit.

Author:

Chia Chen Ciang¹,Jeong Hyo-Mi¹,Lee Jung-Ryul¹,Park Gyuhae²

Affiliation:

1. Department of Aerospace Engineering and LANL-CBNU Engineering Institute Korea; Chonbuk National University; 567 Baekje-daero, Deokjin-gu; Jeonju-si; Jeollabuk-do; 561-756; Korea

2. Engineering Institute, Los Alamos National Laboratory; Los Alamos; NM 87545; USA

Publisher

Wiley

Subject

Mechanics of Materials,Building and Construction,Civil and Structural Engineering

Reference45 articles.

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2. Functionalized composite structures for new generation airframes: a review;Ye;Composites Science and Technology,2005

3. Hsu DK Nondestructive inspection of composite structures: methods and practice Proceedings of 17th World Conference on Nondestructive Testing 2008

4. Ullmann T Schmidt T Hofmann S Jemmali R In-line quality assurance for the manufacturing of carbon fiber reinforced aircraft structures Proceedings of 2nd International Symposium on NDT in Aerospace 2010

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