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Uncertainty quantification of guided wave structural health monitoring for aeronautical composite structures /

Record Type:	Language materials, printed : Monograph/item
Title/Author:	Uncertainty quantification of guided wave structural health monitoring for aeronautical composite structures // Nan Yue, Zahra Sharif Khodaei, M H Ferri Aliabadi.
Author:	Yue, Nan
other author:	Sharif-Khodaei, Z.
Published:	New Jersey :World Scientific, : 2024.,
Description:	xii, 188 p. :ill. (some col.) ; : 24 cm.;
Subject:	Airframes - Testing. -
ISBN:	9781800614697 (hbk.) :

Uncertainty quantification of guided wave structural health monitoring for aeronautical composite structures /
Yue, Nan(Aeronautical engineer).

Uncertainty quantification of guided wave structural health monitoring for aeronautical composite structures /Nan Yue, Zahra Sharif Khodaei, M H Ferri Aliabadi. - New Jersey :World Scientific,2024. - xii, 188 p. :ill. (some col.) ;24 cm. - Computational and experimental methods in structures,vol. 142044-9283 ;. - Computational and experimental methods in structures,vol. 14..

Includes bibliographical references (p. 177-183) and index.

"This monograph presents a Guided Wave Structural Health Monitoring (GWSHM) system for aeronautical composite structures. Particular attention is paid to the development of a reliable and reproducible system with the capability to detect and localise barely visible impact damage (BVID) in Carbon-Fibre Reinforced Polymer (CFRP) structures. A novel sensor installation method that offers ease of application and replacement as well as excellent durability is introduced. Electromechanical Impedance (EMI) is also introduced to assess the durability of the sensor installation methods in simulated aircraft operational conditions, including thermal cycles, fatigue loading and hot-wet conditions. Damage characterisation using GWSHM is described and used to investigate damage in different CFRP structures. Key issues in guided wave-based damage identification are highlighted and addressed, including wave mode and frequency selection, the influence of dynamic load, the validity of simulated damage, and the sensitivity of guided waves to impact damage in different CFRP materials. The influence of temperature on guided wave propagation in anisotropic CFRP structures is described, and a novel baseline reconstruction approach for temperature compensation is presented. Finally, a multi-level hierarchical approach for the quantification of an ultrasonic GWSHM system is presented"--

ISBN: 9781800614697 (hbk.) :NT2828

LCCN: 2023039002Subjects--Topical Terms:

1450124
Airframes
--Testing.

LC Class. No.: TL671.6 / .Y84 2024

Dewey Class. No.: 629.134/31

Uncertainty quantification of guided wave structural health monitoring for aeronautical composite structures /
LDR:02253cam a2200205 a 4500 001 1130360
008 241104s2024 njua b 001 0 eng d
010 $a 2023039002
020 $a 9781800614697 (hbk.) : $c NT2828
020 $z 9781800614703 (ebook for institutions)
020 $z 9781800614710 (ebook for individuals)
040 $a TL $b eng $c TL $d NFU $e AACR2
042 $a pcc
050 0 0 $a TL671.6 $b .Y84 2024
082 0 0 $a 629.134/31
100 1 $a Yue, Nan $c (Aeronautical engineer). $3 1450120
245 1 0 $a Uncertainty quantification of guided wave structural health monitoring for aeronautical composite structures / $c Nan Yue, Zahra Sharif Khodaei, M H Ferri Aliabadi.
260 # $a New Jersey : $b World Scientific, $c 2024.
300 $a xii, 188 p. : $b ill. (some col.) ; $c 24 cm.
490 1 $a Computational and experimental methods in structures, $x 2044-9283 ; $v vol. 14
504 $a Includes bibliographical references (p. 177-183) and index.
520 # $a "This monograph presents a Guided Wave Structural Health Monitoring (GWSHM) system for aeronautical composite structures. Particular attention is paid to the development of a reliable and reproducible system with the capability to detect and localise barely visible impact damage (BVID) in Carbon-Fibre Reinforced Polymer (CFRP) structures. A novel sensor installation method that offers ease of application and replacement as well as excellent durability is introduced. Electromechanical Impedance (EMI) is also introduced to assess the durability of the sensor installation methods in simulated aircraft operational conditions, including thermal cycles, fatigue loading and hot-wet conditions. Damage characterisation using GWSHM is described and used to investigate damage in different CFRP structures. Key issues in guided wave-based damage identification are highlighted and addressed, including wave mode and frequency selection, the influence of dynamic load, the validity of simulated damage, and the sensitivity of guided waves to impact damage in different CFRP materials. The influence of temperature on guided wave propagation in anisotropic CFRP structures is described, and a novel baseline reconstruction approach for temperature compensation is presented. Finally, a multi-level hierarchical approach for the quantification of an ultrasonic GWSHM system is presented"-- $c Provided by publisher.
650 # 0 $a Airframes $x Testing. $3 1450124
650 # 0 $a Structural health monitoring. $3 786458
650 # 0 $a Composite materials $x Testing. $3 636496
650 # 0 $a Measurement uncertainty (Statistics) $3 1111624
650 # 0 $a Wave guides. $3 683888
700 1 # $a Sharif-Khodaei, Z. $q (Zahra). $3 1450121
700 1 # $a Aliabadi Ferri, M. H. $3 1450122
830 0 $a Computational and experimental methods in structures, $v vol. 14. $3 1450123