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
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

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