Reference health
Damage identification in aircraft composite structures: A case study using various non-destructive testing techniques
29/29 checkable references clean · checked 2026-07-23
Every reference with a DOI in the deposited reference list resolved to a known work in Crossref or DataCite at the dated check, and none carried a retraction, withdrawal, or removal notice.
3 without a DOI — not checked. A reference deposited without a DOI is never matched by title or guessed at; it stays outside the checked set, and this line discloses that.
The 29 checked references that resolve
resolves10.1016/j.apacoust.2007.12.012
Acoustic detection of invisible damage in aircraft composite panels
resolves10.1016/j.compstruct.2009.04.014
Detecting barely visible impact damage detection on aircraft composites structures
resolves10.1016/j.compscitech.2008.09.034
Health monitoring of aerospace composite structures – Active and passive approach
resolves10.1016/j.acme.2014.09.007
Low-energy impact behaviour and damage characterization of carbon fibre reinforced polymer and aluminium hybrid laminates
resolves10.1016/j.paerosci.2010.05.001
Structural health monitoring techniques for aircraft composite structures
resolves10.1016/j.compscitech.2014.05.029
Visualization of hidden delamination and debonding in composites through noncontact laser ultrasonic scanning
resolves10.1016/j.ultras.2013.05.007
Guided waves in anisotropic and quasi-isotropic aerospace composites: Three-dimensional simulation and experiment
resolves10.1177/1475921704042697
Embedded-ultrasonics Structural Radar for In Situ Structural Health Monitoring of Thin-wall Structures
resolves10.1016/j.sna.2014.04.027
Multiple damage detection on aircraft composite structures using near-field MUSIC algorithm
resolves10.1016/j.compositesa.2009.09.004
Impact damage detection in composite laminates using nonlinear acoustics
resolves10.1016/j.paerosci.2004.03.001
Aircraft composites assessment by means of transient thermal NDT
resolves10.1016/j.compositesa.2010.09.002
Impact damage in GFRP: New insights with infrared thermography
resolves10.1016/j.infrared.2013.01.004
Automatic detection of impact damage in carbon fiber composites using active thermography
resolves10.1016/j.ijimpeng.2013.12.010
Infrared thermography to evaluate impact damage in glass/epoxy with manufacturing defects
resolves10.1016/j.compositesb.2013.09.036
Characterizing damage in CFRP structures using flash thermography in reflection and transmission configurations
resolves10.1016/j.jsv.2007.12.008
Vibration-based damage detection in an aircraft wing scaled model using principal component analysis and pattern recognition
resolves10.1016/j.ymssp.2007.07.012
Vibration-based skin damage statistical detection and restoration assessment in a stiffened aircraft panel
resolves10.1016/j.compstruct.2006.11.012
Investigation into the use of low cost MEMS accelerometers for vibration based damage detection
resolves10.1016/j.eswa.2012.01.179
Intelligent health monitoring of aerospace composite structures based on dynamic strain measurements
resolves10.1016/j.compositesa.2014.08.010
Smart lightning protection skin for real-time load monitoring of composite aircraft structures under multiple impacts
resolves10.1016/j.ndteint.2005.07.012
Ultrasonic C-Scan and shearography NDI techniques evaluation of impact defects identification
resolves10.1016/j.compstruct.2012.07.028
Analysis of adhesively bonded repairs in composites: Damage detection and prognosis
resolves10.1016/j.compositesa.2013.05.003
Three-dimensional assessment of low velocity impact damage in particle toughened composite laminates using micro-focus X-ray computed tomography and synchrotron radiation laminography
resolves10.1016/j.compstruct.2014.08.010
Vibration-based spatial damage identification in honeycomb-core sandwich composite structures using wavelet analysis
resolves10.1016/j.acme.2014.01.010
Stone impact damage identification in composite plates using modal data and quincunx wavelet analysis
resolves10.4028/www.scientific.net/KEM.569-570.1186
Energy Correlated Damage Indices in Fatigue Crack Extent Quantification
resolves10.1016/j.ymssp.2011.05.015
Damage identification in composite plates using two-dimensional B-spline wavelets
resolves10.12693/APhysPolA.117.878
Studying Efficiency of NDE Techniques Applied to Composite Materials in Aerospace Applications
The 3 references without a DOI — listed, not checked
no DOI — not checked10.1016/j.compstruct.2015.02.080_b0135
no DOI — not checked10.1016/j.compstruct.2015.02.080_b0140
no DOI — not checkedHolschneider M, Kronland-Martinet R, Morlet J, Tchamitchian P. The ’algorithme à trous’. Technical report CPT-88/P.2115, 1988.
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