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Mauricio Donadon
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引用次数
引用次数
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A progressive failure model for composite laminates subjected to low velocity impact damage
MV Donadon, L Iannucci, BG Falzon, JM Hodgkinson, SFM De Almeida
Computers & Structures 86 (11-12), 1232-1252, 2008
4182008
Delamination threshold load for dynamic impact on plates
R Olsson, MV Donadon, BG Falzon
International Journal of solids and structures 43 (10), 3124-3141, 2006
2312006
Ballistic impact simulation of an armour-piercing projectile on hybrid ceramic/fiber reinforced composite armours
D Bürger, AR De Faria, SFM De Almeida, FCL De Melo, MV Donadon
International Journal of Impact Engineering 43, 63-77, 2012
1232012
A 3-D micromechanical model for predicting the elastic behaviour of woven laminates
MV Donadon, BG Falzon, L Iannucci, JM Hodgkinson
Composites Science and Technology 67 (11-12), 2467-2477, 2007
822007
A three-dimensional ply failure model for composite structures
MV Donadon, SFM De Almeida, MA Arbelo, AR de Faria
International Journal of Aerospace Engineering 2009, 2009
682009
Vibration correlation technique for the estimation of real boundary conditions and buckling load of unstiffened plates and cylindrical shells
MA Arbelo, SFM De Almeida, MV Donadon, SR Rett, R Degenhardt, ...
Thin-Walled Structures 79, 119-128, 2014
612014
A numerical study on the impact resistance of composite shells using an energy based failure model
NO Yokoyama, MV Donadon, SFM De Almeida
Composite Structures 93 (1), 142-152, 2010
592010
Flutter suppression of plates using passive constrained viscoelastic layers
AG Cunha-Filho, AMG De Lima, MV Donadon, LS Leão
Mechanical Systems and Signal Processing 79, 99-111, 2016
542016
Intralaminar toughness characterisation of unbalanced hybrid plain weave laminates
MV Donadon, BG Falzon, L Iannucci, JM Hodgkinson
Composites Part A: Applied Science and Manufacturing 38 (6), 1597-1611, 2007
532007
Stiffening effects on the natural frequencies of laminated plates with piezoelectric actuators
MV Donadon, SFM Almeida, AR De Faria
Composites Part B: Engineering 33 (5), 335-342, 2002
462002
Numerical prediction of compression after impact behavior of woven composite laminates
P Mendes, MV Donadon
Composite Structures 113, 476-491, 2014
402014
Assembly of semi-analytical models to address linear buckling and vibration of stiffened composite panels with debonding defect
SGP Castro, MV Donadon
Composite Structures 160, 232-247, 2017
392017
Intraply failure criterion for unidirectional fiber reinforced composites by means of asymptotic homogenization
RQ de Macedo, RTL Ferreira, JM Guedes, MV Donadon
Composite Structures 159, 335-349, 2017
312017
Aeroelastic behavior of composite laminated shells with embedded SMA wires under supersonic flow
MV Donadon, AR de Faria
Aerospace Science and Technology 52, 157-166, 2016
302016
The effect of piezoelectrically induced stress stiffening on the aeroelastic stability of curved composite panels
A Almeida, MV Donadon, AR De Faria, SFM De Almeida
Composite Structures 94 (12), 3601-3611, 2012
302012
Flutter suppression of plates subjected to supersonic flow using passive constrained viscoelastic layers and Golla–Hughes–McTavish method
AG Cunha-Filho, AMG De Lima, MV Donadon, LS Leão
Aerospace Science and Technology 52, 70-80, 2016
292016
Optimization of composite plates subjected to buckling and small mass impact using lamination parameters
RZG Bohrer, SFM de Almeida, MV Donadon
Composite Structures 120, 141-152, 2015
292015
Flutter of stiffened composite panels considering the stiffener’s base as a structural element
SGP Castro, TAM Guimarães, DA Rade, MV Donadon
Composite Structures 140, 36-43, 2016
272016
Moisture effect on the mechanical properties of additively manufactured continuous carbon fiberreinforced Nylonbased thermoplastic
BC Kikuchi, FLS Bussamra, MV Donadon, RTL Ferreira, RCM Sales
Polymer Composites 41 (12), 5227-5245, 2020
252020
ES-PIM applied to buckling of variable angle tow laminates
SGP Castro, MV Donadon, TAM Guimarães
Composite Structures 209, 67-78, 2019
252019
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