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(Referência obtida automaticamente do Web of Science, por meio da informação sobre o financiamento pela FAPESP e o número do processo correspondente, incluída na publicação pelos autores.)

Nonlinear finite element post-flutter analysis of multibay composite panels in supersonic regime

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Pacheco, D. R. Q. ; Marques, F. D. ; Natarajan, S. ; Ferreira, A. J. M.
Número total de Autores: 4
Tipo de documento: Artigo Científico
Fonte: COMPOSITE STRUCTURES; v. 180, p. 883-891, NOV 15 2017.
Citações Web of Science: 7

This study consists of a numerical investigation on the nonlinear flutter oscillations of composite panels on multiple supports (multibay panels) in high supersonic flow. In contrast to what is done in the majority of studies, direct time-domain integration is used here instead of linearized updated mode approximations or modal decomposition techniques. The main goal is to study the interaction between adjacent bays in the nonlinear regime in order to identify aeroelastic phenomena that are not predicted by the usual single-panel approach. Multiple lamination schemes and multibay arrangements are considered, and new important results have been found. In nearly all cases simulated, severe jump discontinuities have been detected in the limit cycle oscillation amplitudes when the dynamic pressure reaches certain values. Such jumps, observed here for the first time, occur due to the nonlinear coupling between neighboring bays and consist of very abrupt amplitude elevations that happen when there are inversions in the motion phase of one or more bays. Furthermore, this study has been able to show that single-panel analysis may be unsafe for structural design as it drastically underestimates the maximum displacements of the bays located in rear (downwind) positions. (C) 2017 Elsevier Ltd. All rights reserved. (AU)

Processo FAPESP: 16/20393-5 - Flutter supersônico não linear de painel usando teoria de deformação-deslocamento de Von Kármán
Beneficiário:Douglas Ramalho Queiroz Pacheco
Linha de fomento: Bolsas no Brasil - Iniciação Científica
Processo FAPESP: 17/01309-6 - Modelo de placa de compósitos laminados não linear de von Kármán para análise de flutter supersônico
Beneficiário:Douglas Ramalho Queiroz Pacheco
Linha de fomento: Bolsas no Exterior - Estágio de Pesquisa - Iniciação Científica