| Author |
Manuscripts |
Pietro Aceti
Politecnico di Milano
|
140 Meso-scale models to analyse the interactions of damage modes in composites laminates
|
Oluwamayokun B. Adetoro
|
138 Opmimization of hybrid composite-metal joints
|
Alessandro Airoldi
Politecnico di Milano
|
140 Meso-scale models to analyse the interactions of damage modes in composites laminates
|
René C. Alderliesten
Aerospace Engineering, TU Delft
|
22 Experimental investigation of planar delamination behavior of composite laminates under out-of –plane loading
36 Towards understanding residual strength and damage evolution in damaged composite laminates
51 Compression after impact fatigue damage growth in CFRP - What does no-growth really mean?
127 Can we predict fatigue crack growth without the help of Paris?
142 On the mechanism of cyclic crack propagation in AA2024 T3 alloy.
148 Combined mechanical and environmental ageing of FRPs - Hygrothermal fatigue case study
|
Sébastien Amiable
airbus
|
52 A new approach to accidental damage on aircraft metallic structure
|
Emiel Amsterdam
NLR
|
32 Back to basics for the fatigue crack growth rate in metallic alloys
|
Dallen Andrew
Hill Engineering
|
56 The A-10 Warthog damage tolerance and residual stresses in transition
29 The engineered residual stress implementation (ERSI) working group
28 The integrated maintenance system (IMx+)
|
Ana Marcia Antunes
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
|
Joana Antunes
|
144 Friction stir welds with enhanced fatigue strength and life via laser peening
|
Takahira Aoki
Department of Aeronautics and Astronautics, The University of Tokyo
|
21 A numerical scheme for fatigue simulation of laminated composites using CZM-XFEM
|
Yuichiro Aoki
Japan Aerospace Exploration Agency
|
130 Optimal design and static load testing of tow-steered aircraft fuselage frames
|
Mariano Arbelo
ITA - Instituto Tecnológico de Aeronáutica
|
146 Crack growth analysis of fiber metal laminates stiffened panels
75 Towards deriving loads spectra representing operational life: Equivalent flight profile versus single flight profiles
|
Hitoshi Arizono
Japan Aerospace Exploration Agency
|
130 Optimal design and static load testing of tow-steered aircraft fuselage frames
|
Moriah Ausherman
SAFE Inc
|
136 Evaluation of cold spray for aircraft repair
|
Andreas Baumann
|
31 Stacking sequence effect on the fatigue behaviour of single-lap shear bonded joints
|
Chuck Babish
United States Airforce
|
5 Digital engineering for improved aircraft structural integrity program execution
|
John Bakuckas
FAA
|
107 Bonded repair size limit studies of representation composite wing panel
45 Test and analysis of fuselage structure to assess Emerging Metallic Structures Technologies
101 Characterization of MSD in emerging metallic structures in fuselage lap joints
|
Andrea Baldi
Leonardo Company
|
114 Assessment on fatigue behavior of AL7475 T7351 subjected to natural corrosion, accelerated corrosion and artificial damages
140 Meso-scale models to analyse the interactions of damage modes in composites laminates
|
Pietro Ballarin
Politecnico di Milano
|
140 Meso-scale models to analyse the interactions of damage modes in composites laminates
|
Rui Bao
Beihang University
|
6 On the theory of aerocraft structural operational integrity control
|
Carlos Antonio Baptista
Engineering School of Lorena, University of São Paulo (EEL/USP)
|
78 Effects of the secondary aging heat treatment T6I4 on fracture toughness and fatigue crack growth resistance of AA7050 alloy
72 Numerical and experimental analyses of the stress field ahead of fatigue cracks in laser-treated AA2198-T851 alloy
|
David Bardenstein
IAI
|
96 Design and experimental validation of a MDAF bonded structure fail safe damage arrest concept
|
Julien Baris
Airbus Operations SAS, France
|
119 Enabling the journey towards Condition Based Maintenance for Airframe
|
Daniel Barroso Vloedgraven
Airbus
|
49 Application of continuum damage mechanics for in-service real fatigue cracking scenarios
|
Martin Bartelt
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
|
Simon Barter
RMIT
|
19 The outcomes of research into nucleation and small fatigue crack growth in aluminium alloy 7085-T7452
7 The lead crack concept history 30 years on
123 Measuring small fatigue crack growth with the aid of marker bands in recrystallized annealed TI6AL4V
|
André Beltempo
National Research Council Canada
|
120 Bell 525 Vertical Fin / Aft Fuselage and Tailboom Composite/Metallic Hybrid Certification Fatigue Testing
|
Marcelo Bertoni
Embraer
|
146 Crack growth analysis of fiber metal laminates stiffened panels
|
Thomas Beumler
Airbus Operations GmbH
|
42 How the holistic approach for GLARE development still brings benefits
|
Davide Biagini
TUDelft
|
36 Towards understanding residual strength and damage evolution in damaged composite laminates
51 Compression after impact fatigue damage growth in CFRP - What does no-growth really mean?
|
Ruopu Bian
|
138 Opmimization of hybrid composite-metal joints
|
Sonia Blayac
Airbus
|
49 Application of continuum damage mechanics for in-service real fatigue cracking scenarios
|
Yan Bombardier
National Research Council Canada
|
24 Development and demonstration of damage tolerance airframe digital twin methods and tools
|
Andrea Brenna
Politecnico di Milano, Dipartimento di Chimica, Materiali e Ingegneria Chimica “G. Natta”
|
114 Assessment on fatigue behavior of AL7475 T7351 subjected to natural corrosion, accelerated corrosion and artificial damages
|
Richard Bulmer
|
44 Some observations to recent full-scale fatigue tests
|
Michael J. Candon
RMIT University
|
116 A prognostics and health management approach for aircraft control surface free-play
|
Joseph Cardinal
Southwest Research Institute
|
37 Past, present, and future stress intensity factor solutions for crack at holes
|
Cauê Carvalho
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
|
Reewanshu Chadha
Federal Aviation Administration
|
107 Bonded repair size limit studies of representation composite wing panel
|
Carlos Chaves
Embraer S.A.
|
45 Test and analysis of fuselage structure to assess Emerging Metallic Structures Technologies
101 Characterization of MSD in emerging metallic structures in fuselage lap joints
115 On the development of statistical knock-down factors for WFD assessment
|
Xianmin Chen
Aircraft Atrength Research Institute
|
86 Low-cycle fatigue property and life prediction model of TC18 titanium alloy material
|
Paul Clark
Southwest Research Institute
|
134 A-10 implementing prognostics with the digital thread
|
Andrew Clark
USAF 417 SCMS/GUEA, Landing Gear Systems
|
110 Tools and methods for landing gear fatigue analysis with surface treatment effects
|
Stephen Clay
|
96 Design and experimental validation of a MDAF bonded structure fail safe damage arrest concept
|
Alain Colle
Bell Helicopter
|
120 Bell 525 Vertical Fin / Aft Fuselage and Tailboom Composite/Metallic Hybrid Certification Fatigue Testing
|
Gabriel Cotrim de Cesare Peinado
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
|
Nathan Crosby
Principal Engineer
|
11 Probabilistic damage tolerance analysis using adaptive multiple importance sampling
|
Lujun Cui
|
138 Opmimization of hybrid composite-metal joints
|
Wei Cui
|
26 Experimental study on the effect of different fatigue loading method on the property of metal cantilever beam
|
Haichao Cui
|
62 Study on fatigue and crack propagation of titanium alloy laminated structure
|
Melanie DUCOFFE
Airbus Operations SAS, France
|
119 Enabling the journey towards Condition Based Maintenance for Airframe
|
Derk Daverschot
Airbus Operations GmbH
|
113 Crack bridging effect in hybrid reinforced fuselage structure
119 Enabling the journey towards Condition Based Maintenance for Airframe
42 How the holistic approach for GLARE development still brings benefits
|
Zvi Deutch
|
96 Design and experimental validation of a MDAF bonded structure fail safe damage arrest concept
|
Rueben Dinakar
Airbus India
|
143 Testing of a cocured compsite frame panel by the applications of vacuum as an alternate to frame bending test
|
BL Dinesh
National Aerospace Laboratories, Bangalore, India
|
143 Testing of a cocured compsite frame panel by the applications of vacuum as an alternate to frame bending test
|
Juliana Diniz Mattos
ITA - Instituto Tecnológico de Aeronáutica
|
75 Towards deriving loads spectra representing operational life: Equivalent flight profile versus single flight profiles
|
Éric Dionne
|
25 Probabilistic lifing of a second oversize hole modification
|
Ben Dixon
Defence Science and Technology Group
|
19 The outcomes of research into nucleation and small fatigue crack growth in aluminium alloy 7085-T7452
|
Dengke Dong
Aircraft Atrength Research Institute
|
86 Low-cycle fatigue property and life prediction model of TC18 titanium alloy material
|
Hongna Dui
|
3 Optimization of selecting strain measurement locations for distributed load recovery from strain measurements
|
Erick Espinar-Mick
Boeing Company
|
107 Bonded repair size limit studies of representation composite wing panel
|
Maria Pia Falaschetti
University of Bologna
|
117 Simulation of crack growth in adhesively bonded joints via cohesive zone models
|
Fabricio Fanton
Embraer
|
45 Test and analysis of fuselage structure to assess Emerging Metallic Structures Technologies
101 Characterization of MSD in emerging metallic structures in fuselage lap joints
|
Pedro Felix
Instituto Tecnologico da Aeronautica
|
146 Crack growth analysis of fiber metal laminates stiffened panels
|
Michea Ferrari
|
121 Practical application of structural risk assessment with SMART|DT
|
Viola Ferrari
|
121 Practical application of structural risk assessment with SMART|DT
|
Michael Fleming
Boeing Company
|
107 Bonded repair size limit studies of representation composite wing panel
|
David Forsyth
NDT Analysis
|
12 NASA NDE fracture critical detectable flaw sizes history and methodology
|
Yuval Freed
Israel Aerospace Industries
|
9 Determination of composite material finite width correction factors using machine learning strategies
|
Erin Fulton
Arconic Technology Center
|
45 Test and analysis of fuselage structure to assess Emerging Metallic Structures Technologies
|
Kotresh Gaddikeri
National Aerospace Laboratories, Bangalore, India
|
143 Testing of a cocured compsite frame panel by the applications of vacuum as an alternate to frame bending test
|
Sarah Galyon Dorman
SAFE Inc
|
136 Evaluation of cold spray for aircraft repair
|
Beth Gamble
Consultant
|
11 Probabilistic damage tolerance analysis using adaptive multiple importance sampling
|
Qi Gang
National Research Council Canada
|
126 Virtual testing of low-velocity impact response of a composite laminate – from analytical to high-fidelity modeling
|
Marc Genest
National Research Council Canada
|
55 Probability of detection of automated tap testing for disbond detection in metallic honeycomb structures
|
Sara Ghiasvand
Politecnico di Milano
|
140 Meso-scale models to analyse the interactions of damage modes in composites laminates
|
Marco Giglio
Politecnico di Milano, Dipartimento di Meccanica
|
114 Assessment on fatigue behavior of AL7475 T7351 subjected to natural corrosion, accelerated corrosion and artificial damages
|
Patrick Golden
US Air Force Research Laboratory
|
106 Fatigue performance and DADT certification of powder-bed additively-manufactured Ti-6Al-4V: defect assessments, EIDS distributions, and inspection limits
|
Guilherme Gomes
Universidade Federal de Itajubá
|
53 Multi-objective sensor placement optimization in helicopter main rotor blade considering the number of sensors and mode shape interpolation
|
Javier Gomez-Escalonilla
Airbus Defence and Space
|
58 A holistic digital twin for service life extension programs
|
Jiadong Gong
QuesTek Innovations LLC
|
33 Using digital twins to accelerate qualification and certification of fatigue critical components
|
Jorge Gonzalez Rubio
Airbus
|
49 Application of continuum damage mechanics for in-service real fatigue cracking scenarios
|
Ben Griffiths
Select Engineering Services
|
110 Tools and methods for landing gear fatigue analysis with surface treatment effects
|
Isaac Grothe
Southwest Research Institute
|
15 Utilizing condemnations, retirements and mods to improve the structural risk analysis of the T-38: turning trash into treasure
|
Michel Guillaume
|
121 Practical application of structural risk assessment with SMART|DT
|
Delon Guo
AVIC Manufacturing Technology Institute
|
27 Influence of microstructure on fatigue small crack growth behaviour of 18NI maraging steel weldment
|
Allan Gustavsson
Saab AB
|
50 Fatigue and damage tolerance testing of Grippen e/f rudder
|
Javier Gómez-Escalonilla Martin
Airbus
|
49 Application of continuum damage mechanics for in-service real fatigue cracking scenarios
|
Joachim Hausmann
|
31 Stacking sequence effect on the fatigue behaviour of single-lap shear bonded joints
|
Andrew Halfpenny
Hottinger Bruel & Kjaer Ltd
|
110 Tools and methods for landing gear fatigue analysis with surface treatment effects
|
Toko Hamaguchi
IHI
|
70 Development of methods for microtexture characterization and dwell fatigue life prediction of dual phase titanium alloys
|
Bryce Harris
USAF
|
38 The inherent need for holistic structural integrity application and progress
|
Daichi Haruyama
IHI
|
84 Consideration of life prediction model for ceramic matrix composite(CMC) with cooling hole
|
Dingni He
|
26 Experimental study on the effect of different fatigue loading method on the property of metal cantilever beam
|
Yuting He
Air Force Engineering University, China
|
6 On the theory of aerocraft structural operational integrity control
|
Sebastian Heimbs
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
|
Johan Birnie Hernández
University of Bologna
|
117 Simulation of crack growth in adhesively bonded joints via cohesive zone models
|
Ryo Higuchi
Department of Aeronautics and Astronautics, The University of Tokyo
|
77 A new method for defects detection in CFRP composites using wavelet analysis and non-contact lamb waves propagation
21 A numerical scheme for fatigue simulation of laminated composites using CZM-XFEM
|
Michelle Hill
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
|
Josh Hodges
Hill Engineering
|
28 The integrated maintenance system (IMx+)
|
David Hoeppner
University of Utah
|
38 The inherent need for holistic structural integrity application and progress
|
Masahiro Hojo
JAXA
|
84 Consideration of life prediction model for ceramic matrix composite(CMC) with cooling hole
|
Tatsuhito Honda
IHI
|
84 Consideration of life prediction model for ceramic matrix composite(CMC) with cooling hole
|
Rong-Can Hong
Department of Aeronautics and Astronautics, The University of Tokyo
|
21 A numerical scheme for fatigue simulation of laminated composites using CZM-XFEM
|
Peter Horst
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
|
Atsushi Hosoi
Waseda University, Japan
|
83 Giga-Cycle Fatigue Properties of Transverse Crack Initiation in Cross Ply CFRP Laminates Using Ultrasonic Fatigue Testingn
|
Naoki Hosoya
Shibaura Institute of Technology
|
77 A new method for defects detection in CFRP composites using wavelet analysis and non-contact lamb waves propagation
|
Laura Hunt
Southwest Research Institute
|
15 Utilizing condemnations, retirements and mods to improve the structural risk analysis of the T-38: turning trash into treasure
|
Christopher Hurst
Manager, Structural Integrity
|
11 Probabilistic damage tolerance analysis using adaptive multiple importance sampling
|
Yuji Ikeda
Kawasaki Heavy Industries, Ltd
|
130 Optimal design and static load testing of tow-steered aircraft fuselage frames
|
Min-Ji Im
|
81 A mobile robotic non-destructive inspection system based on ultrasonic propagation and optical images
|
Yuta Imai
|
112 Fatigue fracture mechanics of selective laser PBF titanium alloy
|
Koichi Inagaki
IHI
|
70 Development of methods for microtexture characterization and dwell fatigue life prediction of dual phase titanium alloys
|
Hiroshi Ishikawa
|
112 Fatigue fracture mechanics of selective laser PBF titanium alloy
|
Sushant Jha
University of Dayton Research Institute
|
106 Fatigue performance and DADT certification of powder-bed additively-manufactured Ti-6Al-4V: defect assessments, EIDS distributions, and inspection limits
|
Reji John
US Air Force Research Laboratory
|
106 Fatigue performance and DADT certification of powder-bed additively-manufactured Ti-6Al-4V: defect assessments, EIDS distributions, and inspection limits
|
Jarno Jokinen
Tampere University
|
48 The development of national MRO capability for a basic trainer aircraft: flight and ground tests
|
Paul Jonas
National Institute for Aviation Research
|
101 Characterization of MSD in emerging metallic structures in fuselage lap joints
|
Michael Jones
RMIT University
|
19 The outcomes of research into nucleation and small fatigue crack growth in aluminium alloy 7085-T7452
|
Kimberli Jones
USAF
|
38 The inherent need for holistic structural integrity application and progress
|
Ilona Kunzler
|
31 Stacking sequence effect on the fatigue behaviour of single-lap shear bonded joints
|
Mikko Kanerva
Tampere University
|
48 The development of national MRO capability for a basic trainer aircraft: flight and ground tests
|
Zlatan Kapidzic
Saab AB
|
50 Fatigue and damage tolerance testing of Grippen e/f rudder
|
Apostolos Karafillis
GE Aerospace
|
133 Fracture mechanics-based approach for anomaly size acceptability of additively manufactured metals
|
Akiko Kasami
|
112 Fatigue fracture mechanics of selective laser PBF titanium alloy
|
Nikolai Kashaev
Helmholtz-Zentrum Hereon
|
122 Retardation of fatigue cracks in welded structures through laser shock peening
|
Itsuki Kawata
IHI
|
70 Development of methods for microtexture characterization and dwell fatigue life prediction of dual phase titanium alloys
|
Sören Keller
Helmholtz-Zentrum Hereon
|
122 Retardation of fatigue cracks in welded structures through laser shock peening
|
Abdul Khadar Syed
Coventry University
|
111 Fatigue performance and cyclic deformation behaviour of titanium TI-6AL-4V additively manufactured by wire + ARC directed energy deposition
|
Muzibur Khan
National Research Council Canada
|
55 Probability of detection of automated tap testing for disbond detection in metallic honeycomb structures
|
Stephen King
Cranfield Univerity
|
128 Machine learning requirements for the airworthiness of structural health monitoring systems in aircraft
|
Yuta Kitamura
IHI
|
70 Development of methods for microtexture characterization and dwell fatigue life prediction of dual phase titanium alloys
|
Dmitrii Klishch
National Research Council Canada
|
55 Probability of detection of automated tap testing for disbond detection in metallic honeycomb structures
|
Benjamin Klusemann
Helmholtz-Zentrum Hereon
|
122 Retardation of fatigue cracks in welded structures through laser shock peening
|
Philip Knoth
|
96 Design and experimental validation of a MDAF bonded structure fail safe damage arrest concept
|
Matthew Kokaly
PartWorks
|
65 Enhanced technology repair for corrosion and fatigue damage in hybrid aerostructure
|
Ingrid Kongshavn
RUAG AG
|
123 Measuring small fatigue crack growth with the aid of marker bands in recrystallized annealed TI6AL4V
|
Tuomas Korteniemi
Patria Aviation Oy
|
48 The development of national MRO capability for a basic trainer aircraft: flight and ground tests
|
Ajay Koshti
NASA
|
12 NASA NDE fracture critical detectable flaw sizes history and methodology
|
Keijo Koski
VTT Technical Research Centre of Finland Ltd
|
95 VIBFAT – Vibration-Induced Fatigue life estimation of the Vertical Tail of the F/A-18 aircraft using virtual sensing
90 QF marker research
|
Iddo Kressel
IAI
|
96 Design and experimental validation of a MDAF bonded structure fail safe damage arrest concept
|
Milan Krkoska
|
142 On the mechanism of cyclic crack propagation in AA2024 T3 alloy.
|
Matthew Krug
US Air Force Research Laboratory
|
106 Fatigue performance and DADT certification of powder-bed additively-manufactured Ti-6Al-4V: defect assessments, EIDS distributions, and inspection limits
|
Jesse van Kuijk
Aerospace Engineering, TU Delft
|
127 Can we predict fatigue crack growth without the help of Paris?
|
Mike Kulak
Diakon Solutions
|
45 Test and analysis of fuselage structure to assess Emerging Metallic Structures Technologies
101 Characterization of MSD in emerging metallic structures in fuselage lap joints
|
Bradley Kuramoto
Leidos
|
38 The inherent need for holistic structural integrity application and progress
|
Luiz G.M. Lise
|
31 Stacking sequence effect on the fatigue behaviour of single-lap shear bonded joints
|
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
|
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
|
Yi-Der Lee
Southwest Research Institute
|
37 Past, present, and future stress intensity factor solutions for crack at holes
|
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
|
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
|
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
|
Siqi Li
|
10 Fatigue life prediction of metallic materials using the Tanaka-Mura-Wu model
30 Microstructure-based computational fatigue life prediction of polycrystalline alloys
|
Lucy Li
National Research Council Canada
|
126 Virtual testing of low-velocity impact response of a composite laminate – from analytical to high-fidelity modeling
|
Lei Li
Aircraft Atrength Research Institute
|
86 Low-cycle fatigue property and life prediction model of TC18 titanium alloy material
|
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
|
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
|
Rong Liu
|
10 Fatigue life prediction of metallic materials using the Tanaka-Mura-Wu model
30 Microstructure-based computational fatigue life prediction of polycrystalline alloys
|
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
|
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
|
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
|
Fabian Nowacki
|
31 Stacking sequence effect on the fatigue behaviour of single-lap shear bonded joints
|
Hiroshi Nakamura
IHI
|
84 Consideration of life prediction model for ceramic matrix composite(CMC) with cooling hole
|
Ömer Namdar
|
113 Crack bridging effect in hybrid reinforced fuselage structure
|
Vesa Nieminen
|
85 Modal testing of vertical tail of F/A-18 Hornet
95 VIBFAT – Vibration-Induced Fatigue life estimation of the Vertical Tail of the F/A-18 aircraft using virtual sensing
|
Daisuke Nishida
Kawasaki Heavy Industries, Ltd
|
130 Optimal design and static load testing of tow-steered aircraft fuselage frames
|
Marv Nuss
Consultant
|
11 Probabilistic damage tolerance analysis using adaptive multiple importance sampling
|
Eugene O'Higgins
Airbus Operations GmbH, Germany
|
119 Enabling the journey towards Condition Based Maintenance for Airframe
|
Juan Ocampo
Associate Professor
|
11 Probabilistic damage tolerance analysis using adaptive multiple importance sampling
|
Ben Ogborne
airbus
|
52 A new approach to accidental damage on aircraft metallic structure
|
Takao Okada
JAXA, Japan
|
118 Research for thermal load and procedure to predict fatigue life up to form a fatigue crack on CFRP/Aluminium hybrid joints
|
Matti Okkonen
VTT
|
135 Optical simulation of scratch repair in F/A-18 transparences
|
Luis Rogério de Oliveira Hein
São Paulo State University
|
78 Effects of the secondary aging heat treatment T6I4 on fracture toughness and fatigue crack growth resistance of AA7050 alloy
|
Greg Olson
Massachusetts Institute of Technology
|
33 Using digital twins to accelerate qualification and certification of fatigue critical components
|
Ryo Omura
|
112 Fatigue fracture mechanics of selective laser PBF titanium alloy
|
Olli Orell
Tampere University
|
48 The development of national MRO capability for a basic trainer aircraft: flight and ground tests
|
Marco Ormellese
Politecnico di Milano, Dipartimento di Chimica, Materiali e Ingegneria Chimica “G. Natta”
|
114 Assessment on fatigue behavior of AL7475 T7351 subjected to natural corrosion, accelerated corrosion and artificial damages
|
Yoshihiro Otani
IHI
|
70 Development of methods for microtexture characterization and dwell fatigue life prediction of dual phase titanium alloys
|
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
|
Francis M.G. Ramírez
|
31 Stacking sequence effect on the fatigue behaviour of single-lap shear bonded joints
|
Martin Raming
Southwest Research Institute
|
134 A-10 implementing prognostics with the digital thread
|
Giuseppe Ratti
Leonardo Helicopter Division
|
114 Assessment on fatigue behavior of AL7475 T7351 subjected to natural corrosion, accelerated corrosion and artificial damages
|
Justin Rausch
SAFE Inc
|
136 Evaluation of cold spray for aircraft repair
|
Manuel J Rebollo
Airbus Defence and Space
|
58 A holistic digital twin for service life extension programs
|
Jiazhi Ren
|
138 Opmimization of hybrid composite-metal joints
|
Guillaume Renaud
|
24 Development and demonstration of damage tolerance airframe digital twin methods and tools
25 Probabilistic lifing of a second oversize hole modification
|
Mathias Renner
|
113 Crack bridging effect in hybrid reinforced fuselage structure
|
Jude Restis
PartWorks
|
65 Enhanced technology repair for corrosion and fatigue damage in hybrid aerostructure
|
Michael Reyer
Aerospace Engineer, Safety Risk Management Section, AIR-633
|
11 Probabilistic damage tolerance analysis using adaptive multiple importance sampling
|
Wagner Rissardo
Embraer S.A.
|
115 On the development of statistical knock-down factors for WFD assessment
|
Ismael Rivero Arevalo
Airbus
|
49 Application of continuum damage mechanics for in-service real fatigue cracking scenarios
|
Marcelo Rodrigues
Embraer
|
45 Test and analysis of fuselage structure to assess Emerging Metallic Structures Technologies
|
John Rogers
National Research Council Canada
|
120 Bell 525 Vertical Fin / Aft Fuselage and Tailboom Composite/Metallic Hybrid Certification Fatigue Testing
|
Simone Romano
GE Avio
|
133 Fracture mechanics-based approach for anomaly size acceptability of additively manufactured metals
|
Rodrigo Ruiz Santos
Airbus
|
49 Application of continuum damage mechanics for in-service real fatigue cracking scenarios
|
Giuseppe Sala
Politecnico di Milano
|
140 Meso-scale models to analyse the interactions of damage modes in composites laminates
|
Fernando Sanchez
Airbus Defence and Space
|
58 A holistic digital twin for service life extension programs
|
Alain Santgerma
airbus
|
52 A new approach to accidental damage on aircraft metallic structure
|
Hayao Sato
IHI
|
84 Consideration of life prediction model for ceramic matrix composite(CMC) with cooling hole
|
Francesco Sausto
GE Avio
|
133 Fracture mechanics-based approach for anomaly size acceptability of additively manufactured metals
|
Mikko Savolainen
|
95 VIBFAT – Vibration-Induced Fatigue life estimation of the Vertical Tail of the F/A-18 aircraft using virtual sensing
|
Michael J. Scott
RMIT University
|
116 A prognostics and health management approach for aircraft control surface free-play
|
Hazen Sedgwick
USAF AFLCMC/WAA
|
134 A-10 implementing prognostics with the digital thread
|
Peyman Shabani
University of Carleton
|
126 Virtual testing of low-velocity impact response of a composite laminate – from analytical to high-fidelity modeling
|
Noam Shemesh
|
96 Design and experimental validation of a MDAF bonded structure fail safe damage arrest concept
|
Gregory Shoales
Center for Aircraft Structural Life Extension (CAStLE)
|
136 Evaluation of cold spray for aircraft repair
|
Mika Siitonen
Finnish Defense Forces Logistics Command
|
135 Optical simulation of scratch repair in F/A-18 transparences
|
Aslak Siljander
VTT
|
90 QF marker research
48 The development of national MRO capability for a basic trainer aircraft: flight and ground tests
135 Optical simulation of scratch repair in F/A-18 transparences
|
Walt Sippel
FAA
|
45 Test and analysis of fuselage structure to assess Emerging Metallic Structures Technologies
101 Characterization of MSD in emerging metallic structures in fuselage lap joints
|
Zbigniew Skorupka
Lukasiewicz Research Network - Institute of Aviation
|
16 Review of aircraft landing gear tests as part of structural testing
|
Martin Skote
Cranfield University
|
128 Machine learning requirements for the airworthiness of structural health monitoring systems in aircraft
|
Luciano Smith
Southwest Research Institute
|
134 A-10 implementing prognostics with the digital thread
|
Brian Smyers
|
96 Design and experimental validation of a MDAF bonded structure fail safe damage arrest concept
|
James Sobotka
Southwest Research Institute
|
37 Past, present, and future stress intensity factor solutions for crack at holes
|
Larissa Sorensen
RUAG AG
|
123 Measuring small fatigue crack growth with the aid of marker bands in recrystallized annealed TI6AL4V
|
TJ Spradlin
USAF AFRL
|
29 The engineered residual stress implementation (ERSI) working group
|
Marcus Stanfield
Southwest Research Institute
|
15 Utilizing condemnations, retirements and mods to improve the structural risk analysis of the T-38: turning trash into treasure
|
Dave Stanley
FAA
|
45 Test and analysis of fuselage structure to assess Emerging Metallic Structures Technologies
|
Kevin Stonaker
|
45 Test and analysis of fuselage structure to assess Emerging Metallic Structures Technologies
101 Characterization of MSD in emerging metallic structures in fuselage lap joints
|
Shaopu Su
Aircraft Atrength Research Institute
|
86 Low-cycle fatigue property and life prediction model of TC18 titanium alloy material
|
Sunao Sugimoto
Japan Aerospace Exploration Agency
|
130 Optimal design and static load testing of tow-steered aircraft fuselage frames
|
Uceu Fuad Hasan Suhuddin
Helmholtz-Zentrum Hereon
|
122 Retardation of fatigue cracks in welded structures through laser shock peening
|
Michael Suits
NASA
|
12 NASA NDE fracture critical detectable flaw sizes history and methodology
|
Qixing Sun
Chinese Aeronautical Establishment
|
87 High strength and ductility across size scales: 3D printed metal materials with microscale heterostructure
|
Shinya Suzukake
|
112 Fatigue fracture mechanics of selective laser PBF titanium alloy
|
Hiroharu Suzuki
Kawasaki Heavy Industries, Ltd
|
130 Optimal design and static load testing of tow-steered aircraft fuselage frames
|
Shin-ichi Takeda
Japan Aerospace Exploration Agency
|
77 A new method for defects detection in CFRP composites using wavelet analysis and non-contact lamb waves propagation
|
Yongzhe Tian
FAA
|
45 Test and analysis of fuselage structure to assess Emerging Metallic Structures Technologies
|
Shota Tonegawa
Shibaura Institute of Technology
|
77 A new method for defects detection in CFRP composites using wavelet analysis and non-contact lamb waves propagation
|
Enrico Troiani
University of Bologna
|
117 Simulation of crack growth in adhesively bonded joints via cohesive zone models
|
Masayuki Tsukada
IHI
|
70 Development of methods for microtexture characterization and dwell fatigue life prediction of dual phase titanium alloys
|
Wenjie Tu
Department of Aerospace Structures & Materials, Faculty of Aerospace Engineering, Delft University of Technology
|
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
|
Aleks Vainionpää
VTT Technical Research Centre of Finland Ltd
|
90 QF marker research
|
Oscar Valencia
Airbus Defence and Space
|
58 A holistic digital twin for service life extension programs
|
Volker Ventzke
Helmholtz-Zentrum Hereon
|
122 Retardation of fatigue cracks in welded structures through laser shock peening
|
Wim J.C. Verhagen
RMIT University
|
116 A prognostics and health management approach for aircraft control surface free-play
|
Tomi Viitanen
|
95 VIBFAT – Vibration-Induced Fatigue life estimation of the Vertical Tail of the F/A-18 aircraft using virtual sensing
|
SR Viswamurthy
National Aerospace Laboratories, Bangalore, India
|
143 Testing of a cocured compsite frame panel by the applications of vacuum as an alternate to frame bending test
|
CH Viswarupachari
National Aerospace Laboratories, Bangalore, India
|
143 Testing of a cocured compsite frame panel by the applications of vacuum as an alternate to frame bending test
|
Xijia WU
|
30 Microstructure-based computational fatigue life prediction of polycrystalline alloys
|
James Walker
NASA
|
12 NASA NDE fracture critical detectable flaw sizes history and methodology
|
Binwen Wang
Aircraft Atrength Research Institute
|
86 Low-cycle fatigue property and life prediction model of TC18 titanium alloy material
|
Bintuan Wang
|
62 Study on fatigue and crack propagation of titanium alloy laminated structure
|
Xin Wang
Carleton University
|
57 Investigation of the tensile/compressive residual stresses in AISI 4340 steel under low-cycle fatigue loading
|
Bin Wang
|
138 Opmimization of hybrid composite-metal joints
|
Yanfei Wang
Peking University
|
87 High strength and ductility across size scales: 3D printed metal materials with microscale heterostructure
|
Wandong Wang
|
97 Bonded prestressed method for fatigue crack repair
|
Mengmeng Wang Wang
Aircraft Strength Research Institute of China
|
63 Rigid loading accelerates full-scale aircraft fatigue test
|
Russell Wanhill
Retired
|
7 The lead crack concept history 30 years on
|
Jacob Warner
USAF A-10 ASIP
|
56 The A-10 Warthog damage tolerance and residual stresses in transition
29 The engineered residual stress implementation (ERSI) working group
|
Peter Webb
|
44 Some observations to recent full-scale fatigue tests
|
Sven Werner
Airbus Operations GmbH
|
143 Testing of a cocured compsite frame panel by the applications of vacuum as an alternate to frame bending test
|
Gary Whelan
QuesTek Innovations LLC
|
33 Using digital twins to accelerate qualification and certification of fatigue critical components
|
X.R Wu
AECC Beijing Institute of Aeronautical Material
|
23 Three-dimensional weight function analyses and stress intensity factors for general surface and corner crack emaninating from circular hole
|
Xijia Wu
National Research Council Canada
|
10 Fatigue life prediction of metallic materials using the Tanaka-Mura-Wu model
|
Wu Xu
Shanghai Jiao Tong University
|
23 Three-dimensional weight function analyses and stress intensity factors for general surface and corner crack emaninating from circular hole
|
Jingfeng Xue
Chinese Aeronautical Establishment
|
87 High strength and ductility across size scales: 3D printed metal materials with microscale heterostructure
|
Naoya Yamada
IHI
|
70 Development of methods for microtexture characterization and dwell fatigue life prediction of dual phase titanium alloys
|
Hongying Yang
|
138 Opmimization of hybrid composite-metal joints
|
Shigeru Yasuda
IHI
|
70 Development of methods for microtexture characterization and dwell fatigue life prediction of dual phase titanium alloys
|
Hoi Yiu
|
44 Some observations to recent full-scale fatigue tests
|
Tomohiro Yokozeki
Department of Aeronautics and Astronautics, The University of Tokyo
|
77 A new method for defects detection in CFRP composites using wavelet analysis and non-contact lamb waves propagation
21 A numerical scheme for fatigue simulation of laminated composites using CZM-XFEM
|
Ryosuke Yoshimura
Kawasaki Heavy Industries, Ltd
|
130 Optimal design and static load testing of tow-steered aircraft fuselage frames
|
Zhijie Yu
Chinese Aeronautical Establishment
|
87 High strength and ductility across size scales: 3D printed metal materials with microscale heterostructure
|
Jianjian Yu
|
26 Experimental study on the effect of different fatigue loading method on the property of metal cantilever beam
|
Nicola Zavatta
University of Bologna
|
117 Simulation of crack growth in adhesively bonded joints via cohesive zone models
|
Xiang Zhang
Coventry University
|
111 Fatigue performance and cyclic deformation behaviour of titanium TI-6AL-4V additively manufactured by wire + ARC directed energy deposition
|
Terry Zhang
Drexel University
|
101 Characterization of MSD in emerging metallic structures in fuselage lap joints
|
Zhong Zhang
|
10 Fatigue life prediction of metallic materials using the Tanaka-Mura-Wu model
30 Microstructure-based computational fatigue life prediction of polycrystalline alloys
|
Bo Zhang
Shanghai Jiao Tong University
|
23 Three-dimensional weight function analyses and stress intensity factors for general surface and corner crack emaninating from circular hole
|
Zhinan Zhang
|
62 Study on fatigue and crack propagation of titanium alloy laminated structure
|
Jipeng Zhang
|
62 Study on fatigue and crack propagation of titanium alloy laminated structure
|
Lei Zhang Zhang
Aircraft Strength Research Institute of China
|
63 Rigid loading accelerates full-scale aircraft fatigue test
|
Wei Zhang Zhang
Aircraft Strength Research Institute of China
|
63 Rigid loading accelerates full-scale aircraft fatigue test
|
Lixin Zhang
|
3 Optimization of selecting strain measurement locations for distributed load recovery from strain measurements
|
Yuan Zhao
|
62 Study on fatigue and crack propagation of titanium alloy laminated structure
|
Tianjiao Zhao
|
62 Study on fatigue and crack propagation of titanium alloy laminated structure
|
Haitao Zhao
AVIC Manufacturing Technology Institute
|
27 Influence of microstructure on fatigue small crack growth behaviour of 18NI maraging steel weldment
|
Jianjun Zheng
Aircraft Strength Research Institute of China
|
63 Rigid loading accelerates full-scale aircraft fatigue test
|
Guiyong Zhong
|
80 Research on structural damage identification methods for aircraft full scale fatigue test
|
Jin Zhou
Chinese Aeronautical Establishment
|
87 High strength and ductility across size scales: 3D printed metal materials with microscale heterostructure
|
