Proceedings

ICAF 2023
Delft, The Netherlands, 2023
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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

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