Zobrazeno 1 - 10 of 27 pro vyhledávání: '"Thiago A.M. Guimarães"'
1
A multidisciplinary design optimization for conceptual design of hybrid-electric aircraft
Autor: André Rezende Dessimoni Carvalho, Roberto M. C. Neto, Thiago A.M. Guimarães, Higor Luis Silva, Gustavo Jorge Resende, Mateus Alves Araújo Cruz, Alexandre Acerra Gil
Publikováno v: Structural and Multidisciplinary Optimization. 64:3505-3526
Aircraft design has become increasingly complex since it depends on technological advances and integration between modern engineering systems. These systems are multidisciplinary, i.e., any process or division of any aircraft design produces effects
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::e6f8dd31a634ecab7cf9986c3d0c3f16
https://doi.org/10.1007/s00158-021-03033-8
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2
Contribuição ao estudo do comportamento dinâmico e aeroelástico de laminados compósitos de rigidez variável
Autor: Thiago A.M. Guimarães
Publikováno v: Repositório Institucional da UFU
Universidade Federal de Uberlândia (UFU)
instacron:UFU
O trabalho de pesquisa realizado trata do comportamento dinâmico e aeroelástico em compósitos laminados de rigidez variável (LCRV). Em virtude dos avanços das técnicas de manufatura de laminados, este tema tem ganhado notoriedade internacional
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::3165a36a0f14de1bb657415073b5724c
https://doi.org/10.14393/ufu.te.2016.163
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6
Aeroelastic tailoring of nonlinear typical section using the method of multiple scales to predict post-flutter stable LCOs
Autor: Flávio D. Marques, Thiago A.M. Guimarães, Leonardo Sanches
Publikováno v: Aerospace Science and Technology
Aerospace Science and Technology, Elsevier, 2019, 90, pp.157-168. ⟨10.1016/j.ast.2019.04.031⟩
Aerospace Science and Technology, 2019, 90, pp.157-168. ⟨10.1016/j.ast.2019.04.031⟩
Most aeroelastic systems suffer from nonlinear behavior. The characterization of nonlinear response in aeroelastic systems is, therefore, a relevant issue. When designing for best performance, for instance, to expand the flutter boundaries, the nonli
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::06f72bfbc96af94a1536bd1da74fc990
https://hal.archives-ouvertes.fr/hal-02122579
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7
ES-PIM applied to buckling of variable angle tow laminates
Autor: Maurício Vicente Donadon, Thiago A.M. Guimarães, Saullo G.P. Castro
Publikováno v: Composite Structures, 209
The increasing need for automatic mesh generation has led to the development of efficient triangulation algorithms that are able to discretize any 2D or 3D domain. Modern finite element formulations based on strain smoothing techniques (SFEM) provide
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f922dd033e1877f6bcd3e7598b5e67c0
http://resolver.tudelft.nl/uuid:ab8296b5-1ad0-4a5a-9600-fc00375bac68
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