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Improving Depth Resolution of Ultrasonic Phased Array Imaging to Inspect Aerospace Composite Structures

Sensors (Basel, Switzerland), 2020-01, Vol.20 (2), p.559

2020

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Lamb-wave-based structural health monitoring technique for inaccessible regions in complex composite structures

Structural control and health monitoring, 2014-05, Vol.21 (5), p.817-832

2014

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Fast, Accurate, and Reliable Detection of Damage in Aircraft Composites by Advanced Synergistic Infrared Thermography and Phased Array Techniques

Applied sciences, 2021-03, Vol.11 (6), p.2778

2021

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Quantitative characterization of interface delamination in composite T-joint using couplant-free Lamb wave methods

Journal of reinforced plastics and composites, 2016-02, Vol.35 (4), p.345-361

2016

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Delamination Size Detection using Time of Flight of Anti-symmetric (Ao) and Mode Converted Ao mode of Guided Lamb Waves

Journal of intelligent material systems and structures, 2010-05, Vol.21 (8), p.817-825

2010

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Delamination Size Detection using Time of Flight of Anti-symmetric (A(o)) and Mode Converted A(o) mode of Guided Lamb Waves

Journal of intelligent material systems and structures, 2010-05, Vol.21 (8), p.817-825

2010

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Materials Characterisation and Structural Health Monitoring of Composite Structures Using Ultrasonic Guided Wave

Journal of Aerospace Sciences and Technologies, 2023-08, p.55-60

2023

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Sizing of delamination using time-of-flight of the fundamental symmetric Lamb modes

Journal of reinforced plastics and composites, 2011-05, Vol.30 (10), p.856-863

2011

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Visualization studies of Lamb wave propagation and interactions with anomalies in composite laminates using air-coupled ultrasonics

AIP Conference Proceedings, 2014, Vol.1581 (1), p.1097

2014

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Ultrasonic Phased Array Imaging Technology for the Inspection of Aerospace Composite Structures

2019 IEEE 5th International Workshop on Metrology for AeroSpace (MetroAeroSpace), 2019, p.203-208

2019

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Lamb-wave-based structural health monitoring technique for inaccessible regions in complex composite structures: LAMB WAVE BASED SHM

Structural control and health monitoring, 2013-09, p.n/a

2013

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Lamb wave based ultrasonic imaging of interface delamination in a composite T-joint

NDT & E international : independent nondestructive testing and evaluation, 2011-10, Vol.44 (6), p.523-530

2011

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Crack Detection in Full Size Cz-Silicon Wafers Using Lamb Wave Air Coupled Ultrasonic Testing (LAC-UT)

Journal of nondestructive evaluation, 2012-03, Vol.31 (1), p.46-55

2012

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Propagation of the Fundamental Symmetric Lamb Mode in a Symmetrically Delaminated Composite Laminate

International journal of vehicle structures and systems, 2012, Vol.4 (3)

2012

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Delamination Size Detection using Time of Flight of Anti-symmetric (A o ) and Mode Converted A o mode of Guided Lamb Waves

Journal of intelligent material systems and structures, 2010-05, Vol.21 (8), p.817-825

2010

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Improving Depth Resolution of Ultrasonic Phased Array Imaging to Inspect Aerospace Composite Structures

Lamb-wave-based structural health monitoring technique for inaccessible regions in complex composite structures

Fast, Accurate, and Reliable Detection of Damage in Aircraft Composites by Advanced Synergistic Infrared Thermography and Phased Array Techniques

Quantitative characterization of interface delamination in composite T-joint using couplant-free Lamb wave methods

Delamination Size Detection using Time of Flight of Anti-symmetric (Ao) and Mode Converted Ao mode of Guided Lamb Waves

Delamination Size Detection using Time of Flight of Anti-symmetric (A(o)) and Mode Converted A(o) mode of Guided Lamb Waves

Materials Characterisation and Structural Health Monitoring of Composite Structures Using Ultrasonic Guided Wave

Sizing of delamination using time-of-flight of the fundamental symmetric Lamb modes

Visualization studies of Lamb wave propagation and interactions with anomalies in composite laminates using air-coupled ultrasonics

Ultrasonic Phased Array Imaging Technology for the Inspection of Aerospace Composite Structures

Lamb-wave-based structural health monitoring technique for inaccessible regions in complex composite structures: LAMB WAVE BASED SHM

Lamb wave based ultrasonic imaging of interface delamination in a composite T-joint

Crack Detection in Full Size Cz-Silicon Wafers Using Lamb Wave Air Coupled Ultrasonic Testing (LAC-UT)

Propagation of the Fundamental Symmetric Lamb Mode in a Symmetrically Delaminated Composite Laminate

Delamination Size Detection using Time of Flight of Anti-symmetric (A o ) and Mode Converted A o mode of Guided Lamb Waves

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