Authors Index

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Author	Manuscripts
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 Mitsubishi Heavy Industries, Ltd.	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

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