Rafael Thiago Luiz Ferreira

Prof. Rafael Thiago Luiz Ferreira


Research Focus & Metrics

Academic Career Length

19Years (2008-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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1 September 2017 in Composites Part B: Engineering
Verified
Journal Article
Closed access
RFRafael Thiago Luiz Ferreira
Rafael Thiago Luiz Ferreira
IAIgor Cardoso Amatte
Igor Cardoso Amatte
TDThiago Assis Dutra
Thiago Assis Dutra
DBDaniel Bürger
Daniel Bürger

18 February 2019 in Journal of the Brazilian Society of Mechanical Sciences and Engineering
Verified
Journal Article
Closed access
TDThiago Assis Dutra
Thiago Assis Dutra
RFRafael Thiago Luiz Ferreira
Rafael Thiago Luiz Ferreira
HRHugo Borelli Resende
Hugo Borelli Resende
AGAlessandro Guimarães
Alessandro Guimarães

1 January 2014 in Composite Structures
Verified
Journal Article
Closed access
RFRafael Thiago Luiz Ferreira
Rafael Thiago Luiz Ferreira
HRHelder C. Rodrigues
Helder C. Rodrigues
JGJosé M. Guedes
José M. Guedes
JHJosé A. Hernandes
José A. Hernandes

1 January 2017 in Composite Structures
Verified
Journal Article
Closed access
RMRafael Quelho de Macedo
Rafael Quelho de Macedo
RFRafael Thiago Luiz Ferreira
Rafael Thiago Luiz Ferreira
JGJosé Miranda Guedes
José Miranda Guedes
MDMaurício Vicente Donadon
Maurício Vicente Donadon

19 February 2020 in Structural and Multidisciplinary Optimization
Verified
Journal Article
Open access
PDF file
RFRafael Thiago Luiz Ferreira
Rafael Thiago Luiz Ferreira
IAIan A. Ashcroft
Ian A. Ashcroft
The Hashin’s strength criteria are usually employed in first ply failure and damage-onset analysis of fibre-reinforced composites. This work presents optimality conditions of local material orientations for these criteria, in terms of principal stresses and material strength parameters. Each criterion (matrix tensile/compressive, fibre tensile/compressive modes) has its conditions separately derived, analytically, based on a fixed stress field assumption. The conditions found show that orientations which coincide and do not coincide with principal stress directions may minimise local failure indices. These solutions are employed in a proposed algorithm, named HA-OCM (Hashin Optimality Criteria Method), which selectively satisfies the matrix failure modes (either tensile or compressive), iteratively and finite element-wise in composites. It is demonstrated that the HA-OCM is able to design single-layer plane structures with improved failure loads in comparison with designs following only maximum (in absolute) principal stress orientations. Results show that the material orientations have a trend to end up either aligned or at 90° with maximum in absolute principal stress directions. Global optima for compliance are, however, not guaranteed. To give an idea of gains in terms of failure loads, some HA-OCM designs show improvements of 71% and 140%, for example, in comparison with principal stress design.

1 September 2021 in Composites Science and Technology
Verified
Journal Article
Open access
TDThiago Assis Dutra
Thiago Assis Dutra
RFRafael Thiago Luiz Ferreira
Rafael Thiago Luiz Ferreira
HRHugo Borelli Resende
Hugo Borelli Resende
BBBrina Jane Blinzler
Brina Jane Blinzler
LALeif Asp
Leif Asp