Topology optimization including a model of the layer-by-layer additive manufacturing process

GA Haveroth, CJ Thore, MR Correa, RF Ausas… - Computer methods in …, 2022 - Elsevier
A topology optimization formulation including a model of the layer-by-layer additive
manufacturing (AM) process is considered. Defined as a multi-objective minimization …

On the convergence of the primal hybrid finite element method on quadrilateral meshes

G Taraschi, MR Correa - Applied Numerical Mathematics, 2022 - Elsevier
We consider the approximation of a second order elliptic equation (Darcy problem) by using
the Primal Hybrid Finite Element Method on quadrilateral meshes. We present new results in …

Optimal H (div) flux approximations from the Primal Hybrid Finite Element Method on quadrilateral meshes

MR Correa, G Taraschi - Computer Methods in Applied Mechanics and …, 2022 - Elsevier
In this work, we propose and analyze an element-wise H (div, Ω)-conforming computational
strategy to post-process the flux vector from the approximated solution of a second-order …

[PDF][PDF] On the accuracy of finite element approximations of elliptic problems with heterogeneous coefficients

G Taraschi, AS Pinto, CO Faria… - XLII Ibero-Latin …, 2021 - publicacoes.softaliza.com.br
On the accuracy of finite element approximations of elliptic problems with heterogeneous
coefficients Page 1 On the accuracy of finite element approximations of elliptic problems …

Numerical analysis of forward and inverse fluid mechanics problems

C Carcamo - 2021 - research.rug.nl
In this thesis, we have proposed and analysed PDE-based fluid models such as Navier-
Stokes, Oseen and nonlinear Darcy. We have proved their solvability using the classical …

Airfoil lift finite element computations using H1 (Ω) and H (div, Ω) approximation spaces

SGF Cordeiro, CHC Puga… - Ibero-Latin …, 2024 - publicacoes.softaliza.com.br
Computing the lift generated by an airfoil is crucial in aircraft design, especially for aircraft
performance prediction, aircraft stability/control, and optimization of airfoil shape for …