Authors Index

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Author	Manuscripts
Risto Laakso VTT, Helsinki	95 VIBFAT – Vibration-Induced Fatigue life estimation of the Vertical Tail of the F/A-18 aircraft using virtual sensing 90 QF marker research 50 Fatigue and damage tolerance testing of Grippen e/f rudder
Tim Labik Drexel University	107 Bonded repair size limit studies of representation composite wing panel
Jeremy Laliberte Carleton University	126 Virtual testing of low-velocity impact response of a composite laminate – from analytical to high-fidelity modeling 57 Investigation of the tensile/compressive residual stresses in AISI 4340 steel under low-cycle fatigue loading
Patrick Langlois Bell Helicopter	120 Bell 525 Vertical Fin / Aft Fuselage and Tailboom Composite/Metallic Hybrid Certification Fatigue Testing
Lea Lecointre The University of Tokyo	77 A new method for defects detection in CFRP composites using wavelet analysis and non-contact lamb waves propagation
Yi-Der Lee Southwest Research Institute	37 Past, present, and future stress intensity factor solutions for crack at holes
Jung-Ryul Lee Korea Advanced Institute of Science and Technology	81 A mobile robotic non-destructive inspection system based on ultrasonic propagation and optical images 47 Development of AI to diagnose depth direction defect in continuous fiber 3D printed CFRP composite based on laser ultrasonic testing
Kyu Jin Lee Korea Advanced Institute of Science and Technology (KAIST)	46 Robotic-based laser ultrasonic non-destructive testing of 3D-printed continuous fiber reinforced flight control surface
Jung Ryul Lee Korea Advanced Institute of Science and Technology (KAIST)	46 Robotic-based laser ultrasonic non-destructive testing of 3D-printed continuous fiber reinforced flight control surface
Kyu-Jin Lee Korea Advanced Institute of Science and Technology	47 Development of AI to diagnose depth direction defect in continuous fiber 3D printed CFRP composite based on laser ultrasonic testing
Rik-Jan Lemmen Airbus Operations GmbH	42 How the holistic approach for GLARE development still brings benefits
Oleg Levinski Defence Science and Technology Group	116 A prognostics and health management approach for aircraft control surface free-play
Lei Li Aircraft Atrength Research Institute	86 Low-cycle fatigue property and life prediction model of TC18 titanium alloy material
Siqi Li Carleton University	10 Fatigue life prediction of metallic materials using the Tanaka-Mura-Wu model
Lucy Li National Research Council Canada	126 Virtual testing of low-velocity impact response of a composite laminate – from analytical to high-fidelity modeling
Min Liao	16 Review of aircraft landing gear tests as part of structural testing 24 Development and demonstration of damage tolerance airframe digital twin methods and tools 25 Probabilistic lifing of a second oversize hole modification 121 Practical application of structural risk assessment with SMART\|DT
Yunfei Liao	26 Experimental study on the effect of different fatigue loading method on the property of metal cantilever beam
Milton Sergio Lima Photonics Division, Institute for Advanced Studies (IEAv/DCTA)	72 Numerical and experimental analyses of the stress field ahead of fatigue cracks in laser-treated AA2198-T851 alloy
John Lin Boeing Company	107 Bonded repair size limit studies of representation composite wing panel
Jianhong Lin Aircraft Strength Research Institute (ASRI), Chinese Aeronautical Establishment	18 Considerations to reduce the uncertainties of fatigue failures in large aircraft structures
Jan Erik Lindbäck Saab AB	50 Fatigue and damage tolerance testing of Grippen e/f rudder
Eric Lindgren US Air Force Research Laboratory	67 Aviation-based nondestructive evaluation data analytics
Luiz Lise ar engineers	31 Stacking sequence effect on the fatigue behavior of single lap shear bonded joints
Rong Liu Carleton University	10 Fatigue life prediction of metallic materials using the Tanaka-Mura-Wu model
Dongliang Liu	3 Optimization of selecting strain measurement locations for distributed load recovery from strain measurements
Xiaodong Liu	80 Research on structural damage identification methods for aircraft full scale fatigue test
Sauli Liukkonen Technical Research Centre of Finland Ltd	48 The development of national MRO capability for a basic trainer aircraft: flight and ground tests
Alex Lukatsky	96 Design and experimental validation of a MDAF bonded structure fail safe damage arrest concept
Tim Luplow TU Braunschweig - Institute of Aircraft Design and Lightweight Structures (IFL)	71 Influence of the layer thickness on the very high cycle fatigue behaviour of composite materials

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