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
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

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