| 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
|
