Authors Index

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Author	Manuscripts
Ligeia Paletti Royal NLR	8 Structural integrity as enabler towards sustainability in aviation 142 On the mechanism of cyclic crack propagation in AA2024 T3 alloy.
Shaozhen Pan	80 Research on structural damage identification methods for aircraft full scale fatigue test
Shashank Pant National Research Council Canada	55 Probability of detection of automated tap testing for disbond detection in metallic honeycomb structures
Hyeon-Gyu Park 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
Peter Parker NASA	12 NASA NDE fracture critical detectable flaw sizes history and methodology
John-Alan Pascoe TUDelft	36 Towards understanding residual strength and damage evolution in damaged composite laminates 22 Experimental investigation of planar delamination behavior of composite laminates under out-of –plane loading 51 Compression after impact fatigue damage growth in CFRP - What does no-growth really mean?
João Paulo Pascon Engineering School of Lorena, University of São Paulo (EEL/USP)	72 Numerical and experimental analyses of the stress field ahead of fatigue cracks in laser-treated AA2198-T851 alloy
Marian Patrick Carleton University	57 Investigation of the tensile/compressive residual stresses in AISI 4340 steel under low-cycle fatigue loading
Samara Cristiny de Paula University of Sao Paulo, Brazil	78 Effects of the secondary aging heat treatment T6I4 on fracture toughness and fatigue crack growth resistance of AA7050 alloy
João Pereira	53 Multi-objective sensor placement optimization in helicopter main rotor blade considering the number of sensors and mode shape interpolation
Suresh Perinpanayagam University of York	128 Machine learning requirements for the airworthiness of structural health monitoring systems in aircraft
Valentin Perruchoud Department of Engineering Structures, Faculty of Civil Engineering and Geosciences, TU Delft, Delft, Netherlands	148 Combined mechanical and environmental ageing of FRPs - Hygrothermal fatigue case study
Andrew Perry GE Aerospace	133 Fracture mechanics-based approach for anomaly size acceptability of additively manufactured metals
Robert Pilarczyk Hill Engineering	28 The integrated maintenance system (IMx+)
Jouni Pirtola Patria Aviation Oy	48 The development of national MRO capability for a basic trainer aircraft: flight and ground tests
Rob Plaskitt Hottinger Bruel & Kjaer Ltd	110 Tools and methods for landing gear fatigue analysis with surface treatment effects 111 Fatigue performance and cyclic deformation behaviour of titanium TI-6AL-4V additively manufactured by wire + ARC directed energy deposition
William Prosser NASA	12 NASA NDE fracture critical detectable flaw sizes history and methodology

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