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Artigo de periodico
Stacking sequence optimization in composite tubes under internal pressure based on genetic algorithm accounting for progressive damage (2017)
Almeida Júnior, José Humberto Santos; Ribeiro, Marcelo Leite ; Tita, Volnei ; Amico, Sandro Campos
Source: Composite Structures. Unidade: EESC
Subjects: MÉTODO DOS ELEMENTOS FINITOS, ALGORITMOS GENÉTICOS, MATERIAIS COMPÓSITOS, FALHA, ENGENHARIA AERONÁUTICA
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ABNT
ALMEIDA JÚNIOR, José Humberto Santos et al. Stacking sequence optimization in composite tubes under internal pressure based on genetic algorithm accounting for progressive damage. Composite Structures, v. 178, p. 20-26, 2017Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2017.07.054. Acesso em: 17 nov. 2025.
APA
Almeida Júnior, J. H. S., Ribeiro, M. L., Tita, V., & Amico, S. C. (2017). Stacking sequence optimization in composite tubes under internal pressure based on genetic algorithm accounting for progressive damage. Composite Structures, 178, 20-26. doi:10.1016/j.compstruct.2017.07.054
NLM
Almeida Júnior JHS, Ribeiro ML, Tita V, Amico SC. Stacking sequence optimization in composite tubes under internal pressure based on genetic algorithm accounting for progressive damage [Internet]. Composite Structures. 2017 ; 178 20-26.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2017.07.054
Vancouver
Almeida Júnior JHS, Ribeiro ML, Tita V, Amico SC. Stacking sequence optimization in composite tubes under internal pressure based on genetic algorithm accounting for progressive damage [Internet]. Composite Structures. 2017 ; 178 20-26.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2017.07.054
Artigo de periodico
Nonlinear finite element post-flutter analysis of multibay composite panels in supersonic regime (2017)
Pacheco, D. R. Q.; Marques, Flavio Donizeti ; Natarajan, S.; Ferreira, A. J. M.
Source: Composite Structures. Unidade: EESC
Subjects: AEROELASTICIDADE DE AERONAVES, MÉTODO DOS ELEMENTOS FINITOS, VIBRAÇÕES DE AERONAVES, ENGENHARIA MECÂNICA
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ABNT
PACHECO, D. R. Q. et al. Nonlinear finite element post-flutter analysis of multibay composite panels in supersonic regime. Composite Structures, v. 180, p. 883-891, 2017Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2017.08.058. Acesso em: 17 nov. 2025.
APA
Pacheco, D. R. Q., Marques, F. D., Natarajan, S., & Ferreira, A. J. M. (2017). Nonlinear finite element post-flutter analysis of multibay composite panels in supersonic regime. Composite Structures, 180, 883-891. doi:10.1016/j.compstruct.2017.08.058
NLM
Pacheco DRQ, Marques FD, Natarajan S, Ferreira AJM. Nonlinear finite element post-flutter analysis of multibay composite panels in supersonic regime [Internet]. Composite Structures. 2017 ; 180 883-891.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2017.08.058
Vancouver
Pacheco DRQ, Marques FD, Natarajan S, Ferreira AJM. Nonlinear finite element post-flutter analysis of multibay composite panels in supersonic regime [Internet]. Composite Structures. 2017 ; 180 883-891.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2017.08.058
Artigo de periodico
Damage modeling for carbon fiber/epoxy filament wound composite tubes under radial compression (2017)
Almeida Júnior, José Humberto Santos; Ribeiro, Marcelo Leite ; Tita, Volnei ; Amico, Sandro Campos
Source: Composite Structures. Unidade: EESC
Subjects: ANÁLISE NUMÉRICA, FALHA, MÉTODO DOS ELEMENTOS FINITOS
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
ALMEIDA JÚNIOR, José Humberto Santos et al. Damage modeling for carbon fiber/epoxy filament wound composite tubes under radial compression. Composite Structures, v. 160, n. Ja 2017, p. 204-210, 2017Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2016.10.036. Acesso em: 17 nov. 2025.
APA
Almeida Júnior, J. H. S., Ribeiro, M. L., Tita, V., & Amico, S. C. (2017). Damage modeling for carbon fiber/epoxy filament wound composite tubes under radial compression. Composite Structures, 160( Ja 2017), 204-210. doi:10.1016/j.compstruct.2016.10.036
NLM
Almeida Júnior JHS, Ribeiro ML, Tita V, Amico SC. Damage modeling for carbon fiber/epoxy filament wound composite tubes under radial compression [Internet]. Composite Structures. 2017 ; 160( Ja 2017): 204-210.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2016.10.036
Vancouver
Almeida Júnior JHS, Ribeiro ML, Tita V, Amico SC. Damage modeling for carbon fiber/epoxy filament wound composite tubes under radial compression [Internet]. Composite Structures. 2017 ; 160( Ja 2017): 204-210.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2016.10.036
Artigo de periodico
Low-density polyethylene waste/recycled wood composites (2017)
Moreno, Diego David Pinzon; Saron, Clodoaldo
Source: Composite Structures. Unidade: EEL
Subjects: MATERIAIS COMPÓSITOS, FIBRAS VEGETAIS, PINHEIRO, RESÍDUOS FLORESTAIS
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ABNT
MORENO, Diego David Pinzon e SARON, Clodoaldo. Low-density polyethylene waste/recycled wood composites. Composite Structures, v. 176, p. 1152-1157, 2017Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2017.05.076. Acesso em: 17 nov. 2025.
APA
Moreno, D. D. P., & Saron, C. (2017). Low-density polyethylene waste/recycled wood composites. Composite Structures, 176, 1152-1157. doi:10.1016/j.compstruct.2017.05.076
NLM
Moreno DDP, Saron C. Low-density polyethylene waste/recycled wood composites [Internet]. Composite Structures. 2017 ;176 1152-1157.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2017.05.076
Vancouver
Moreno DDP, Saron C. Low-density polyethylene waste/recycled wood composites [Internet]. Composite Structures. 2017 ;176 1152-1157.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2017.05.076
Artigo de periodico
Zig-Zag effect without degrees of freedom in linear and non linear analysis of laminated plates and shells (2017)
Coda, Humberto Breves ; Paccola, Rodrigo Ribeiro ; Carrazedo, Rogério
Source: Composite Structures. Unidade: EESC
Subjects: ANÁLISE NÃO LINEAR DE ESTRUTURAS, LAMINADOS, PLACAS, ESTRUTURAS
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ABNT
CODA, Humberto Breves e PACCOLA, Rodrigo Ribeiro e CARRAZEDO, Rogério. Zig-Zag effect without degrees of freedom in linear and non linear analysis of laminated plates and shells. Composite Structures, v. 161, p. 32-50, 2017Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2016.10.129. Acesso em: 17 nov. 2025.
APA
Coda, H. B., Paccola, R. R., & Carrazedo, R. (2017). Zig-Zag effect without degrees of freedom in linear and non linear analysis of laminated plates and shells. Composite Structures, 161, 32-50. doi:10.1016/j.compstruct.2016.10.129
NLM
Coda HB, Paccola RR, Carrazedo R. Zig-Zag effect without degrees of freedom in linear and non linear analysis of laminated plates and shells [Internet]. Composite Structures. 2017 ; 161 32-50.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2016.10.129
Vancouver
Coda HB, Paccola RR, Carrazedo R. Zig-Zag effect without degrees of freedom in linear and non linear analysis of laminated plates and shells [Internet]. Composite Structures. 2017 ; 161 32-50.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2016.10.129
Artigo de periodico
Evolutionary-based aeroelastic tailoring of stiffened laminate composite panels in supersonic flow regime (2017)
Marques, Flavio Donizeti ; Natarajan, S.; Ferreira, António J. M.
Source: Composite Structures. Unidade: EESC
Subjects: MATERIAIS COMPÓSITOS, LAMINADOS, PAINÉIS, AEROELASTICIDADE DE AERONAVES
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
MARQUES, Flavio Donizeti e NATARAJAN, S. e FERREIRA, António J. M. Evolutionary-based aeroelastic tailoring of stiffened laminate composite panels in supersonic flow regime. Composite Structures, v. 167, p. 30-37, 2017Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2017.01.062. Acesso em: 17 nov. 2025.
APA
Marques, F. D., Natarajan, S., & Ferreira, A. J. M. (2017). Evolutionary-based aeroelastic tailoring of stiffened laminate composite panels in supersonic flow regime. Composite Structures, 167, 30-37. doi:10.1016/j.compstruct.2017.01.062
NLM
Marques FD, Natarajan S, Ferreira AJM. Evolutionary-based aeroelastic tailoring of stiffened laminate composite panels in supersonic flow regime [Internet]. Composite Structures. 2017 ; 167 30-37.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2017.01.062
Vancouver
Marques FD, Natarajan S, Ferreira AJM. Evolutionary-based aeroelastic tailoring of stiffened laminate composite panels in supersonic flow regime [Internet]. Composite Structures. 2017 ; 167 30-37.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2017.01.062
Artigo de periodico
A novel fiber optimization method based on normal distribution function with continuously varying fiber path (2017)
Kiyono, César Yukishigue; Silva, Emílio Carlos Nelli ; Reddy, J. N.
Source: Composite Structures. Unidade: EP
Assunto: MATERIAIS COMPÓSITOS DE FIBRAS
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ABNT
KIYONO, César Yukishigue e SILVA, Emílio Carlos Nelli e REDDY, J. N. A novel fiber optimization method based on normal distribution function with continuously varying fiber path. Composite Structures, v. 160, p. 503-515, 2017Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2016.10.064. Acesso em: 17 nov. 2025.
APA
Kiyono, C. Y., Silva, E. C. N., & Reddy, J. N. (2017). A novel fiber optimization method based on normal distribution function with continuously varying fiber path. Composite Structures, 160, 503-515. doi:10.1016/j.compstruct.2016.10.064
NLM
Kiyono CY, Silva ECN, Reddy JN. A novel fiber optimization method based on normal distribution function with continuously varying fiber path [Internet]. Composite Structures. 2017 ; 160 503-515.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2016.10.064
Vancouver
Kiyono CY, Silva ECN, Reddy JN. A novel fiber optimization method based on normal distribution function with continuously varying fiber path [Internet]. Composite Structures. 2017 ; 160 503-515.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2016.10.064
Artigo de periodico
Triangular based prismatic finite element for the analysis of orthotropic laminated beams, plates and shells (2017)
Carrazedo, Rogério ; Coda, Humberto Breves
Source: Composite Structures. Unidade: EESC
Subjects: MÉTODO DOS ELEMENTOS FINITOS, VIGAS, LAMINADOS, ESTRUTURAS
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
CARRAZEDO, Rogério e CODA, Humberto Breves. Triangular based prismatic finite element for the analysis of orthotropic laminated beams, plates and shells. Composite Structures, v. 168, p. 234-246, 2017Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2017.02.027. Acesso em: 17 nov. 2025.
APA
Carrazedo, R., & Coda, H. B. (2017). Triangular based prismatic finite element for the analysis of orthotropic laminated beams, plates and shells. Composite Structures, 168, 234-246. doi:10.1016/j.compstruct.2017.02.027
NLM
Carrazedo R, Coda HB. Triangular based prismatic finite element for the analysis of orthotropic laminated beams, plates and shells [Internet]. Composite Structures. 2017 ; 168 234-246.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2017.02.027
Vancouver
Carrazedo R, Coda HB. Triangular based prismatic finite element for the analysis of orthotropic laminated beams, plates and shells [Internet]. Composite Structures. 2017 ; 168 234-246.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2017.02.027

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