Sérgio Frascino Müller de Almeida
University of São Paulo
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Journal of Intelligent Material Systems and Structures | 1996
Sérgio Frascino Müller de Almeida; António Marcos de Oliveira Costa; Sidney Luiz Alessi Carrara
A finite element formulation for solving the scalar wave equation is described. The proposed formulation leads to an eigenvalue problem defined in terms of positive definite matrices. Therefore, convergence of the two first eigenvectors/eigenvalues to modes LP01 and LP1, and their correspondent propagation constants is guaranteed. A computer code was written to implement the finite element formulation. The software assembles the matrix eigenvalue problem and solves it either with the sub-space iteration method or the power iteration method. The software also computes the coordinates of the centroid of the modal field distribution of each mode. The finite element model can be used to assess the effects of bending the optical fiber about an arbitrary axis on the guided light. The numerical analysis accounts for the mechanical deformation of the fiber cross section and the variation of the refractive index profile due to all strain components present in pure bending. A comparison of the analyses of light propagation in the fiber under unstrained and strained conditions enables one to estimate the bend sensitivity of a two-mode fiber interferometer. Numerical results confirm experimental observations that a small asymmetry of the core index profile may lead to a significant bend sensitivity of a two-mode fiber interferometer. The present model was used to assess the influence of several parameters on the bend sensitivity of an asymmetrical core two-mode fiber interferometer. The excellent agreement between the numerical and experimental results indicates that this numerical model is a reliable tool to analyze the effect of bending strains in twomode fiber interferometers.
AIAA Journal | 2016
Felipe Franzoni; Sérgio Frascino Müller de Almeida; Clovis Augusto Eça Ferreira
This paper proposes a numerical approach to estimate the dynamic behavior of a typical aeronautical aluminum box-beam structure liable to buckling. The methodology is based on a nonlinear finite element model and an experimental modal analysis procedure. The finite element model deals with the coupled nonlinear static and dynamic problems in two steps: 1)xa0determining the static equilibrium considering geometrical nonlinearities, and 2)xa0solving for a linear small-amplitude free-vibration problem based on the tangential stiffness matrix from the current static equilibrium. To illustrate the proposed method, a finite element model is built for a simple supported box beam under a uniaxial compression load with different degrees of eccentricity. The numerical results are correlated with an experimental modal analysis procedure in pre- and postbuckling regimes. Based on this comparison, an updated model is proposed for adjusting the shape and magnitude of the initial imperfections based on linear buckling modes...
Composite Structures | 2017
C.B. York; Sérgio Frascino Müller de Almeida
Archive | 2018
Yvan Bovolenta Murta; C.B. York; Sérgio Frascino Müller de Almeida
Composite Structures | 2018
C.B. York; Sérgio Frascino Müller de Almeida
CEAS Aeronautical Journal | 2018
Gunther Moors; Christos Kassapoglou; Sérgio Frascino Müller de Almeida; Clovis Augusto Eça Ferreira
Archive | 2017
C.B. York; Sérgio Frascino Müller de Almeida
Composites Part A-applied Science and Manufacturing | 2017
C.B. York; Sérgio Frascino Müller de Almeida
Archive | 2016
C.B. York; Sérgio Frascino Müller de Almeida
Journal of the Optical Society of America | 1995
Sidney Luiz Alessi Carrara; Sérgio Frascino Müller de Almeida; C. Eric Covington; James N. Blake