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Flavio Bussamra
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Year
Three‐dimensional hybrid‐Trefftz stress elements
JAT De Freitas, FLS Bussamra
International Journal for Numerical Methods in Engineering 47 (5), 927-950, 2000
502000
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
332020
Hybrid-Trefftz stress elements for three-dimensional elastoplasticity
FLS Bussamra, PM Pimenta, JAT Freitas
Computer Assisted Mechanics and Engineering Sciences 8 (2-3), 235-246, 2001
292001
The postbuckling behaviour of adhesively bonded stiffened panels subjected to in-plane shear loading
APG Villani, MV Donadon, MA Arbelo, P Rizzi, CV Montestruque, ...
Aerospace Science and Technology 46, 30-41, 2015
192015
A new metamodel for reinforced panels under compressive loads and its application to the fuselage conception
AT Neto, FLDES BUSSAMRA, HADECE SILVA
Latin American Journal of Solids and Structures 11 (2), 223-244, 2014
152014
Hybrid quasi-Trefftz 3-D finite elements for laminated composite plates
FLS Bussamra, EL Neto, DS Raimundo Jr
Computers & structures 92, 185-192, 2012
142012
Flexible aircraft simulation validation with flight test data
AB Guimarães Neto, GC Barbosa, JA Paulino, RM Bertolin, JSM Nunes, ...
AIAA Journal 61 (1), 285-304, 2023
112023
Static loads evaluation in a flexible aircraft using high-fidelity fluid–structure iteration tool (E2-FSI): extended version
AA Verri, FLS Bussamra, KC de Morais, GG Becker, CES Cesnik, ...
Journal of the Brazilian Society of Mechanical Sciences and Engineering 42, 1-9, 2020
102020
Linear translaminar fracture characterization of additive manufactured continuous carbon fiber reinforced thermoplastic
WM Lamin, FLS Bussamra, RTL Ferreira, RCM Sales, JE Baldo Jr
Journal of Thermoplastic Composite Materials 36 (3), 1328-1355, 2023
92023
An enhanced random vibration and fatigue model for printed circuit boards
BC Braz, FLS Bussamra
Latin American Journal of Solids and Structures 14, 2402-2422, 2017
92017
Finite element procedure for stress amplification factor recovering in a representative volume of composite materials
PC Plaisant, FLS Bussamra, FK Arakaki
Journal of Aerospace Technology and Management 3 (3), 239-250, 2011
92011
Multidisciplinary methods for wing flight shape analysis—effect of the geometric nonlinear structure for static pull-up
AA Verri, CT Jorge, AF Bizarro, FLS Bussamra, HNS Júnior, CES Cesnik
31st congress of the international council of the aeronautical sciences—ICAS, 2018
82018
Effects of geometric nonlinearity on flexible wing structures
AP Perroni, FLS Bussamra
Journal of Aircraft 58 (1), 85-97, 2021
72021
Three dimensional hybrid‐Trefftz stress finite elements for plates and shells
PHC Martins, FLS Bussamra, E Lucena Neto
International Journal for Numerical Methods in Engineering 113 (11), 1676-1696, 2018
72018
Simulation of stress concentration problems by hexahedral hybrid-Trefftz finite element models
FLS Bussamra, E Lucena Neto, WM Ponciano
Computer Modeling in Engineering & Sciences 99 (3), 255-272, 2014
72014
Skin buckling of fuselages under compression
P Soares, FAC Monteiro, EL Neto, FLS Bussamra
COBEM, 8976-8985, 2013
72013
Experimental determination of unmanned aircraft inertial properties
F Bussamra, CMM Vilchez, JC Santos
Proceedings of 3rd CTA-DLR Workshop on Data Analysis and Flight Control, 14-16, 2009
72009
Validity of the assumption of small deformations in aircraft with different levels of structural flexibility
AB Guimarães Neto, FJ Silvestre, FL Cardoso-Ribeiro, FLS Bussamra, ...
International Forum on Aeroelasticity and Structural Dynamics (IFASD), 2017
62017
Equações constitutivas do concreto baseadas na mecânica do dano contínuo
FLS Bussamra, PM Pimenta
61994
Static loads evaluation in a flexible aircraft using high fidelity fluid–structure iteration tool (E2-FSI)
AA Verri, KC Morais, FLS Bussamra, GG Becker, CES Cesnik
31st congress of the international council of the aeronautical sciences—ICAS, 2018
52018
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