Núbia Nale Silveira
Aeronáutica
Composite numberMode (statistics)Composite laminatesStrain rateComposite materialEpoxyDomain (software engineering)Work (electrical)Materials scienceReliability engineeringJoint (geology)Adhesive bondingPlain weaveContext (language use)Characterization (materials science)Stress concentrationCarbon compositesMixed modeCyclic loadingStrain energy release rateFocus (computing)Computer scienceFracture (geology)CarbonStress intensity factorFracture mechanicsTerm (time)AdhesiveParis' lawDelaminationWater coolingSplit-Hopkinson pressure barFracture toughnessToughness
11Publications
3H-index
19Citations
Publications 11
Newest
#1Chris RijsdijkH-Index: 1
Last. Tiedo TingaH-Index: 20
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In the present paper, the potential of using ship sensor data for achieving smart maintenance of naval ships is discussed. In modern ships, a lot of installations and equipment contain sensors that monitor and register the operation of these systems. This work will exemplify the value of the (long term) collection and analysis of sensor data. This will mainly focus on assessing the present performance or condition of systems and the detection of faults or failures, but also on the longer term am...
Abstract Adhesive bonding technologies exhibit several advantages over conventional mechanical fasteners which include lower weight, reduced stress concentration in the adherents and excellent fatigue properties allowing the design of smooth surface contour and damage tolerant aerostructures. The overall structural performance of the composite joint depends on several factors related to the manufacturing process, such as surface preparation procedure, adhesive type, aging effects, and deficiency...
2 CitationsSource
#1Rita de Cássia Mendonça Sales (ITA: Instituto Tecnológico de Aeronáutica)H-Index: 6
#2A.F. de SousaH-Index: 1
Last. Maurício Vicente Donadon (ITA: Instituto Tecnológico de Aeronáutica)H-Index: 15
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Abstract Adhesive joints exhibit several advantages over conventional joints based on mechanical fasteners such as more uniform stress distribution, enhanced fatigue performance, stiffer connection, lower weight, smooth surface countor. However, the influence of environmental effects related to temperature and moisture absorption on the mechanical performance of these types of composite joints are not yet fully understood. This work investigates the hygrothermal effects on fracture toughness of ...
5 CitationsSource
Source
#1Núbia Nale Silveira (Aeronáutica)H-Index: 3
Last. Maurício Vicente Donadon (Aeronáutica)H-Index: 15
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2 CitationsSource
3 CitationsSource
#1Marcos Yutaka Shiino (UNESP: Sao Paulo State University)H-Index: 7
#2Francis Mariana González Ramírez (Aeronáutica)H-Index: 2
Last. Maurício Vicente Donadon (Aeronáutica)H-Index: 15
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#1Luiz Fernando Martins Leite (ITA: Instituto Tecnológico de Aeronáutica)H-Index: 1
#1Bruno Martins Leite (ITA: Instituto Tecnológico de Aeronáutica)H-Index: 1
Last. Núbia Nale Silveira (ITA: Instituto Tecnológico de Aeronáutica)H-Index: 3
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Abstract This paper presents an experimental and numerical study focused on the mode-I intralaminar toughness characterization of a woven carbon/epoxy composite loaded in compression and subjected to high strain rates. Simulations for non-standardized Single Edge Notch Bending (SENB) and Double Edge Notch (DEN) specimens were carried out using a continuum damage mechanics based failure model implemented as an user defined material model within ABAQUS software. A Finite Element Model was used in ...
8 CitationsSource
Last. Núbia Nale SilveiraH-Index: 3
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#1Francis GonzalezH-Index: 1
Last. Felipe Parise GarpelliH-Index: 2
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