Proceedings

ICAF 2023
Delft, The Netherlands, 2023
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Authors Index

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Author Manuscripts
Yu-E M
66 Effect of the build direction on defect distribution and crack initiation of LPBF TI6AL4V
Shinya MIyazaki
IHI
70 Development of methods for microtexture characterization and dwell fatigue life prediction of dual phase titanium alloys
Frank Machado
Embraer
75 Towards deriving loads spectra representing operational life: Equivalent flight profile versus single flight profiles
Kimberly Maciejewski
Arconic
101 Characterization of MSD in emerging metallic structures in fuselage lap joints
Ben Madsen
General Atomics Systems Integration
110 Tools and methods for landing gear fatigue analysis with surface treatment effects
Ben Main
Defence Science and Technology Group
19 The outcomes of research into nucleation and small fatigue crack growth in aluminium alloy 7085-T7452
Catalin Mandache
National Research Council Canada
55 Probability of detection of automated tap testing for disbond detection in metallic honeycomb structures
Andrea Manes
Politecnico di Milano, Dipartimento di Meccanica
114 Assessment on fatigue behavior of AL7475 T7351 subjected to natural corrosion, accelerated corrosion and artificial damages
Ugo Mariani
Leonardo Helicopter Division
114 Assessment on fatigue behavior of AL7475 T7351 subjected to natural corrosion, accelerated corrosion and artificial damages
Rebeca Martínez Perez
Airbus
49 Application of continuum damage mechanics for in-service real fatigue cracking scenarios
Sayaka Maruta
112 Fatigue fracture mechanics of selective laser PBF titanium alloy
Pier Marzocca
RMIT University
116 A prognostics and health management approach for aircraft control surface free-play
Paul Mattheij
Airbus Operations GmbH
42 How the holistic approach for GLARE development still brings benefits
Craig McClung
Southwest Research Institute
37 Past, present, and future stress intensity factor solutions for crack at holes
Felipe Mello
53 Multi-objective sensor placement optimization in helicopter main rotor blade considering the number of sensors and mode shape interpolation
Emanuele Mesiani
Leonardo Company
140 Meso-scale models to analyse the interactions of damage modes in composites laminates
Daniele Mezzanzanica
Leonardo Helicopter Division
114 Assessment on fatigue behavior of AL7475 T7351 subjected to natural corrosion, accelerated corrosion and artificial damages
Antero Miettinen
Patria Aviation Oy
48 The development of national MRO capability for a basic trainer aircraft: flight and ground tests
Harry Millwater
Professor
11 Probabilistic damage tolerance analysis using adaptive multiple importance sampling
Haroun El Mir
Cranfield University
128 Machine learning requirements for the airworthiness of structural health monitoring systems in aircraft
Masakatsu Mita
Shibaura Institute of Technology
77 A new method for defects detection in CFRP composites using wavelet analysis and non-contact lamb waves propagation
Loris Molent
Molent Aerostructures, Melbourne, Australia
7 The lead crack concept history 30 years on
Yasmine Mosleh
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
Sohrob Mottaghi
General Engineer, Structures and Materials Section - ANG-E281
11 Probabilistic damage tolerance analysis using adaptive multiple importance sampling

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