| 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
20 SWISS TITANIUM RESEARCH EXPERIMENTS ON THE CLASSIC HORNET (STRETCH)
|
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
|
Carmel Matias
Fatigue and Damage Tolerance Engineer, Israel Aerospace Industries
|
54 TI-6AL-4V additive manufacturing mechanical properties as indication to measure of quality
|
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
|
Aki Mäyrä
VTT
|
135 Optical simulation of scratch repair in F/A-18 transparences
|
