| 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
|
