Authors Index

[A] [B] [C] [D] [E] [F] [G] [H] [I] [J] [K] [L] [M] [N] [O] [P] [R] [S] [T] [V] [W] [X] [Y] [Z]

Author	Manuscripts
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

[A] [B] [C] [D] [E] [F] [G] [H] [I] [J] [K] [L] [M] [N] [O] [P] [R] [S] [T] [V] [W] [X] [Y] [Z]