Maurício Vicente Donadon
Instituto Tecnológico de Aeronáutica
Composite numberAeroelasticityEngineeringMode (statistics)AerodynamicsFinite element methodComposite laminatesComposite materialEpoxyCompression (physics)ScatteringMaterials scienceFlutterDamage mechanicsFracture mechanicsStructural engineeringDelaminationBucklingStress (mechanics)Fracture toughness
123Publications
15H-index
1,113Citations
Publications 123
Newest
This paper describes a classical laminate theory-based constitutive model for portraying thermoplastic composites’ mechanical properties and the development of residual stresses during consolidatio...
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#1Gefferson Silva (ITA: Instituto Tecnológico de Aeronáutica)H-Index: 2
#2Maurício Vicente Donadon (ITA: Instituto Tecnológico de Aeronáutica)H-Index: 15
Last. Flávio Silvestre (Technical University of Berlin)H-Index: 2
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Abstract This study performs an experimental and numerical investigation on the nonlinear aeroelastic response of cantilever high-aspect-ratio beam-like wings with a ballast at their free tips, emulating the effects of a store. As an extent, the effects of different chord-wise ballast positions are experimentally examined for two highly flexible rectangular wings. Furthermore, the numerical model proposed brings forward a nonlinear finite element beam model accounting for aerodynamic nonlinearit...
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#1Felipe Ruivo Fuga (ITA: Instituto Tecnológico de Aeronáutica)
#2Maurício Vicente Donadon (ITA: Instituto Tecnológico de Aeronáutica)H-Index: 15
Abstract Despite composite materials presenting a viable design solution for structural weight savings, their low resistance to impact damage portraits a potential drawback. This work presents a study on the compressive pre-loading effects on Low Velocity Impact, LVI, for composite laminated plates. Despite the absence of a standard testing procedure accounting for pre-load effects, a test rig was designed specifically for LVI on pre-loaded plates while preserving ASTM D7136M-15 guidelines for t...
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#1Gabriel Prosofsky de Araujo (ITA: Instituto Tecnológico de Aeronáutica)H-Index: 1
#2Maurício Vicente Donadon (ITA: Instituto Tecnológico de Aeronáutica)H-Index: 15
Last. Rita de Cássia Mendonça Sales (ITA: Instituto Tecnológico de Aeronáutica)H-Index: 6
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Abstract This work presents an experimental study on the mechanical behaviour of thermoplastic polyarlyetherketone (PAEK) based composite laminates reinforced with woven carbon fibres, subjected to high strain rates under compression loading. The specimens were tested using a Split Hopkinson Pressure Bar (SHPB). The tests covered the working temperatures and stress envelopes of −54 °C, RT (25 °C), and 80 °C, each tested at six different off-axis angles. The high-speed imaging system was used to ...
1 CitationsSource
#1A.G. Cunha-FilhoH-Index: 4
#2Yvon Briend (INSA Lyon: Institut national des sciences Appliquées de Lyon)H-Index: 2
Last. Maurício Vicente DonadonH-Index: 15
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Abstract In the open literature, many authors have used the fractional calculus in conjunction with the finite element method to model certain viscoelastic systems. The so-named fractional derivative model may be a better option for transient analyses of systems containing viscoelastic materials due to its causal behavior and its capability to fit accurately the viscoelastic damping properties and to represent properly their fading memory. However, depending on the situation, it leads to costly ...
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#1Thyago Santos Braga (INPE: National Institute for Space Research)H-Index: 1
#2Nirton C. S. Vieira (UNIFESP: Federal University of São Paulo)H-Index: 11
Last. Evaldo José Corat (INPE: National Institute for Space Research)H-Index: 33
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Abstract This study introduces fast manufactured (4−5 hours) vertical aligned carbon nanotubes/polydimethylsiloxane (VACNT/PDMS) stretchable sensor for aircraft structures and polymer composites. The VACNT growth method from thermal CVD with camphor and ferrocene precursors create a dense and homogeneous CNT structure with many ohmic conducting paths that surpass any more resistive tunneling phenomena. The extensive AC/DC piezoresistive performance investigation shows ohmic conduction. The VACNT...
1 CitationsSource
#1Sérgio Augusto Capasciutti de Oliveira (ITA: Instituto Tecnológico de Aeronáutica)H-Index: 2
#2Maurício Vicente Donadon (ITA: Instituto Tecnológico de Aeronáutica)H-Index: 15
A constitutive damage model is proposed in order to investigate the crushing response of crossply and 0 ° plies composite laminates, using a VUMAT subroutine implemented in ABAQUS/Explicit. This da...
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1 CitationsSource
#1Francis Mariana González Ramírez (ITA: Instituto Tecnológico de Aeronáutica)H-Index: 2
#2Felipe Parise Garpelli (ITA: Instituto Tecnológico de Aeronáutica)H-Index: 2
Last. Maurício Vicente Donadon (ITA: Instituto Tecnológico de Aeronáutica)H-Index: 15
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Abstract Aeronautic structures are exposed to a great variety of temperatures and humid environments during service. Nowadays, it is known that the combined influence of moisture and temperature induces further detrimental effects on the fatigue behavior of bonded joints when compared to the influence of each isolated condition. The effect of hygrothermal pre-conditioning on the fatigue delamination growth onset of different bonded technologies was investigated. This paper provides a material da...
2 CitationsSource
#1Thiago de Souza Siqueira Versiani (ITA: Instituto Tecnológico de Aeronáutica)H-Index: 4
Last. Alessandro GuimarãesH-Index: 1
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Abstract Recent aircraft are increasingly presenting unconventional wing configurations, resulting in unusual aeroelastic responses and consequently giving rise to different technological strategies to enhance aeroelastic stability. Among them, the technique of stress stiffening by piezoelectric actuation emerged as a promising technological solution to improve the aeroelastic stability of structures with both ends axially constrained. Therefore, an aeroelastic model employing smart composite be...
3 CitationsSource