Filtros : "Almeida Júnior, José Humberto Santos" Limpar

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  • Source: Theoretical and Applied Fracture Mechanics. Unidade: EESC

    Subjects: LAMINADOS, MATERIAIS COMPÓSITOS, MÉTODO DOS ELEMENTOS FINITOS, ENGENHARIA AERONÁUTICA

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      CHRISTOFF, Bruno Guilherme et al. Multiscale modelling of composite laminates with voids through the direct FE2 method. Theoretical and Applied Fracture Mechanics, v. 131, p. 1-14, 2024Tradução . . Disponível em: https://dx.doi.org/10.1016/j.tafmec.2024.104424. Acesso em: 03 jun. 2024.
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      Christoff, B. G., Almeida Júnior, J. H. S., Ribeiro, M. L., Maciel, M. M. Á. D., Guedes, R. M., & Tita, V. (2024). Multiscale modelling of composite laminates with voids through the direct FE2 method. Theoretical and Applied Fracture Mechanics, 131, 1-14. doi:10.1016/j.tafmec.2024.104424
    • NLM

      Christoff BG, Almeida Júnior JHS, Ribeiro ML, Maciel MMÁD, Guedes RM, Tita V. Multiscale modelling of composite laminates with voids through the direct FE2 method [Internet]. Theoretical and Applied Fracture Mechanics. 2024 ; 131 1-14.[citado 2024 jun. 03 ] Available from: https://dx.doi.org/10.1016/j.tafmec.2024.104424
    • Vancouver

      Christoff BG, Almeida Júnior JHS, Ribeiro ML, Maciel MMÁD, Guedes RM, Tita V. Multiscale modelling of composite laminates with voids through the direct FE2 method [Internet]. Theoretical and Applied Fracture Mechanics. 2024 ; 131 1-14.[citado 2024 jun. 03 ] Available from: https://dx.doi.org/10.1016/j.tafmec.2024.104424
  • Source: Composites Science and Technology. Unidade: EESC

    Subjects: MATERIAIS COMPÓSITOS, IMPRESSÃO 3-D, TOPOLOGIA, MANUFATURA ADITIVA, ENGENHARIA AERONÁUTICA

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      ALMEIDA JÚNIOR, José Humberto Santos et al. A concurrent fibre orientation and topology optimisation framework for 3D-printed fibre-reinforced composites. Composites Science and Technology, v. 232, p. 1-15, 2023Tradução . . Disponível em: https://doi.org/10.1016/j.compscitech.2022.109872. Acesso em: 03 jun. 2024.
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      Almeida Júnior, J. H. S., Christoff, B. G., Tita, V., & St-Pierre, L. (2023). A concurrent fibre orientation and topology optimisation framework for 3D-printed fibre-reinforced composites. Composites Science and Technology, 232, 1-15. doi:10.1016/j.compscitech.2022.109872
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      Almeida Júnior JHS, Christoff BG, Tita V, St-Pierre L. A concurrent fibre orientation and topology optimisation framework for 3D-printed fibre-reinforced composites [Internet]. Composites Science and Technology. 2023 ; 232 1-15.[citado 2024 jun. 03 ] Available from: https://doi.org/10.1016/j.compscitech.2022.109872
    • Vancouver

      Almeida Júnior JHS, Christoff BG, Tita V, St-Pierre L. A concurrent fibre orientation and topology optimisation framework for 3D-printed fibre-reinforced composites [Internet]. Composites Science and Technology. 2023 ; 232 1-15.[citado 2024 jun. 03 ] Available from: https://doi.org/10.1016/j.compscitech.2022.109872
  • Source: Engineering Structures. Unidade: EESC

    Subjects: TOPOLOGIA, HOMOGENEIZAÇÃO, ENGENHARIA AERONÁUTICA

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      CHRISTOFF, Bruno Guilherme e ALMEIDA JÚNIOR, José Humberto Santos e CARDOSO, Eduardo L. A multiscale topology optimisation framework for hollow spheres as cellular materials. Engineering Structures, v. 284, p. 1-13, 2023Tradução . . Disponível em: https://doi.org/10.1016/j.engstruct.2023.115990. Acesso em: 03 jun. 2024.
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      Christoff, B. G., Almeida Júnior, J. H. S., & Cardoso, E. L. (2023). A multiscale topology optimisation framework for hollow spheres as cellular materials. Engineering Structures, 284, 1-13. doi:10.1016/j.engstruct.2023.115990
    • NLM

      Christoff BG, Almeida Júnior JHS, Cardoso EL. A multiscale topology optimisation framework for hollow spheres as cellular materials [Internet]. Engineering Structures. 2023 ; 284 1-13.[citado 2024 jun. 03 ] Available from: https://doi.org/10.1016/j.engstruct.2023.115990
    • Vancouver

      Christoff BG, Almeida Júnior JHS, Cardoso EL. A multiscale topology optimisation framework for hollow spheres as cellular materials [Internet]. Engineering Structures. 2023 ; 284 1-13.[citado 2024 jun. 03 ] Available from: https://doi.org/10.1016/j.engstruct.2023.115990
  • Source: Thin-Walled Structures. Unidade: EESC

    Subjects: MECÂNICA DO DANO, MÉTODO DOS ELEMENTOS FINITOS, ENGENHARIA MECÂNICA

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      FERREIRA, Gregório Felipe Oliveira et al. A finite element unified formulation for composite laminates in bending considering progressive damage. Thin-Walled Structures, v. 172, p. 1-13, 2022Tradução . . Disponível em: https://doi.org/10.1016/j.tws.2021.108864. Acesso em: 03 jun. 2024.
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      Ferreira, G. F. O., Almeida Júnior, J. H. S., Ribeiro, M. L., Ferreira, A. J. M., & Tita, V. (2022). A finite element unified formulation for composite laminates in bending considering progressive damage. Thin-Walled Structures, 172, 1-13. doi:10.1016/j.tws.2021.108864
    • NLM

      Ferreira GFO, Almeida Júnior JHS, Ribeiro ML, Ferreira AJM, Tita V. A finite element unified formulation for composite laminates in bending considering progressive damage [Internet]. Thin-Walled Structures. 2022 ; 172 1-13.[citado 2024 jun. 03 ] Available from: https://doi.org/10.1016/j.tws.2021.108864
    • Vancouver

      Ferreira GFO, Almeida Júnior JHS, Ribeiro ML, Ferreira AJM, Tita V. A finite element unified formulation for composite laminates in bending considering progressive damage [Internet]. Thin-Walled Structures. 2022 ; 172 1-13.[citado 2024 jun. 03 ] Available from: https://doi.org/10.1016/j.tws.2021.108864
  • Source: Composites Part B. Unidade: EESC

    Subjects: PROCESSOS DE FABRICAÇÃO, FLAMBAGEM, ENGENHARIA AERONÁUTICA

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      ALMEIDA JÚNIOR, José Humberto Santos et al. Design, modeling, optimization, manufacturing and testing of variable-angle filament-wound cylinders. Composites Part B, v. 225, p. 1-17, 2021Tradução . . Disponível em: https://doi.org/10.1016/j.compositesb.2021.109224. Acesso em: 03 jun. 2024.
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      Almeida Júnior, J. H. S., St-Pierre, L., Zhihua, W., Ribeiro, M. L., Tita, V., Amico, S. C., & Castro, S. G. P. (2021). Design, modeling, optimization, manufacturing and testing of variable-angle filament-wound cylinders. Composites Part B, 225, 1-17. doi:10.1016/j.compositesb.2021.109224
    • NLM

      Almeida Júnior JHS, St-Pierre L, Zhihua W, Ribeiro ML, Tita V, Amico SC, Castro SGP. Design, modeling, optimization, manufacturing and testing of variable-angle filament-wound cylinders [Internet]. Composites Part B. 2021 ; 225 1-17.[citado 2024 jun. 03 ] Available from: https://doi.org/10.1016/j.compositesb.2021.109224
    • Vancouver

      Almeida Júnior JHS, St-Pierre L, Zhihua W, Ribeiro ML, Tita V, Amico SC, Castro SGP. Design, modeling, optimization, manufacturing and testing of variable-angle filament-wound cylinders [Internet]. Composites Part B. 2021 ; 225 1-17.[citado 2024 jun. 03 ] Available from: https://doi.org/10.1016/j.compositesb.2021.109224
  • Source: Proceedings of BCCM 5. Conference titles: Brazilian Conference on Composite Materials - BCCM. Unidade: EESC

    Subjects: MATERIAIS COMPÓSITOS, MÉTODO DOS ELEMENTOS FINITOS

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      MACIEL, Maísa Milanez Ávila et al. A methodology for modeling variable axial laminates: a case study of a uniformly loaded circular plate. 2021, Anais.. São Carlos, SP: EESC/USP, 2021. Disponível em: https://repositorio.usp.br/directbitstream/0c8ccce2-ca31-481a-b1b9-7f62c1a18f56/2929-8022-1-PB.pdf. Acesso em: 03 jun. 2024.
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      Maciel, M. M. Á., Almeida Júnior, J. H. S., Ribeiro, M. L., & Tita, V. (2021). A methodology for modeling variable axial laminates: a case study of a uniformly loaded circular plate. In Proceedings of BCCM 5. São Carlos, SP: EESC/USP. Recuperado de https://repositorio.usp.br/directbitstream/0c8ccce2-ca31-481a-b1b9-7f62c1a18f56/2929-8022-1-PB.pdf
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      Maciel MMÁ, Almeida Júnior JHS, Ribeiro ML, Tita V. A methodology for modeling variable axial laminates: a case study of a uniformly loaded circular plate [Internet]. Proceedings of BCCM 5. 2021 ;[citado 2024 jun. 03 ] Available from: https://repositorio.usp.br/directbitstream/0c8ccce2-ca31-481a-b1b9-7f62c1a18f56/2929-8022-1-PB.pdf
    • Vancouver

      Maciel MMÁ, Almeida Júnior JHS, Ribeiro ML, Tita V. A methodology for modeling variable axial laminates: a case study of a uniformly loaded circular plate [Internet]. Proceedings of BCCM 5. 2021 ;[citado 2024 jun. 03 ] Available from: https://repositorio.usp.br/directbitstream/0c8ccce2-ca31-481a-b1b9-7f62c1a18f56/2929-8022-1-PB.pdf
  • Source: Thin-Walled Structures. Unidade: EESC

    Subjects: MÉTODO DOS ELEMENTOS FINITOS, LAMINADOS, AERONÁUTICA

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      FERREIRA, Gregório Felipe Oliveira et al. Development of a finite element via unified formulation: implementation as a user element subroutine to predict stress profiles in composite plates. Thin-Walled Structures, v. 157, p. 1-19, 2020Tradução . . Disponível em: https://doi.org/10.1016/j.tws.2020.107107. Acesso em: 03 jun. 2024.
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      Ferreira, G. F. O., Almeida Júnior, J. H. S., Ribeiro, M. L., Ferreira, A. J. M., & Tita, V. (2020). Development of a finite element via unified formulation: implementation as a user element subroutine to predict stress profiles in composite plates. Thin-Walled Structures, 157, 1-19. doi:10.1016/j.tws.2020.107107
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      Ferreira GFO, Almeida Júnior JHS, Ribeiro ML, Ferreira AJM, Tita V. Development of a finite element via unified formulation: implementation as a user element subroutine to predict stress profiles in composite plates [Internet]. Thin-Walled Structures. 2020 ; 157 1-19.[citado 2024 jun. 03 ] Available from: https://doi.org/10.1016/j.tws.2020.107107
    • Vancouver

      Ferreira GFO, Almeida Júnior JHS, Ribeiro ML, Ferreira AJM, Tita V. Development of a finite element via unified formulation: implementation as a user element subroutine to predict stress profiles in composite plates [Internet]. Thin-Walled Structures. 2020 ; 157 1-19.[citado 2024 jun. 03 ] Available from: https://doi.org/10.1016/j.tws.2020.107107
  • Source: Composite Structures. Unidade: EESC

    Subjects: MATERIAIS COMPÓSITOS, MÉTODO DOS ELEMENTOS FINITOS

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      ALMEIDA JÚNIOR, José Humberto Santos et al. Buckling optimization of composite cylinders for axial compression: A design methodology considering a variable-axial fiber layout. Composite Structures, v. 222, p. 1-12, 2019Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2019.110928. Acesso em: 03 jun. 2024.
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      Almeida Júnior, J. H. S., Bittrich, L., Jansen, E., Tita, V., & Spickenheuer, A. (2019). Buckling optimization of composite cylinders for axial compression: A design methodology considering a variable-axial fiber layout. Composite Structures, 222, 1-12. doi:10.1016/j.compstruct.2019.110928
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      Almeida Júnior JHS, Bittrich L, Jansen E, Tita V, Spickenheuer A. Buckling optimization of composite cylinders for axial compression: A design methodology considering a variable-axial fiber layout [Internet]. Composite Structures. 2019 ; 222 1-12.[citado 2024 jun. 03 ] Available from: https://doi.org/10.1016/j.compstruct.2019.110928
    • Vancouver

      Almeida Júnior JHS, Bittrich L, Jansen E, Tita V, Spickenheuer A. Buckling optimization of composite cylinders for axial compression: A design methodology considering a variable-axial fiber layout [Internet]. Composite Structures. 2019 ; 222 1-12.[citado 2024 jun. 03 ] Available from: https://doi.org/10.1016/j.compstruct.2019.110928
  • Source: Proceedings of CNB2019. Conference titles: International Conference on Thin-Walled Structures - ICTWS. Unidade: EESC

    Subjects: ESTRUTURA DE AERONAVES, MÉTODO DOS ELEMENTOS FINITOS, ENGENHARIA AERONÁUTICA

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      RIBEIRO, Marcelo Leite et al. Progressive failure analysis of composite cylinders under transverse impact via high order finite element formulation: through-the-thickness stress profiles evaluation. 2018, Anais.. Lisboa, Portugal: Escola de Engenharia de São Carlos, Universidade de São Paulo, 2018. Disponível em: https://repositorio.usp.br/directbitstream/4e5aa62d-b68b-42f8-a789-28f54d186fe3/trabalho%2012%20-%20%20Progressive%20failure%20analysis%20of%20composite%20cylinders%20under%20transverse%20impact%20via%20high%20order%20finite%20element%20formulation%20through-the-thickness%20stress%20profiles%20evaluation%20%28ICTWS%202018%29_removed.pdf. Acesso em: 03 jun. 2024.
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      Ribeiro, M. L., Almeida Júnior, J. H. S., Garcia, J. D. A., & Tita, V. (2018). Progressive failure analysis of composite cylinders under transverse impact via high order finite element formulation: through-the-thickness stress profiles evaluation. In Proceedings of CNB2019. Lisboa, Portugal: Escola de Engenharia de São Carlos, Universidade de São Paulo. Recuperado de https://repositorio.usp.br/directbitstream/4e5aa62d-b68b-42f8-a789-28f54d186fe3/trabalho%2012%20-%20%20Progressive%20failure%20analysis%20of%20composite%20cylinders%20under%20transverse%20impact%20via%20high%20order%20finite%20element%20formulation%20through-the-thickness%20stress%20profiles%20evaluation%20%28ICTWS%202018%29_removed.pdf
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      Ribeiro ML, Almeida Júnior JHS, Garcia JDA, Tita V. Progressive failure analysis of composite cylinders under transverse impact via high order finite element formulation: through-the-thickness stress profiles evaluation [Internet]. Proceedings of CNB2019. 2018 ;[citado 2024 jun. 03 ] Available from: https://repositorio.usp.br/directbitstream/4e5aa62d-b68b-42f8-a789-28f54d186fe3/trabalho%2012%20-%20%20Progressive%20failure%20analysis%20of%20composite%20cylinders%20under%20transverse%20impact%20via%20high%20order%20finite%20element%20formulation%20through-the-thickness%20stress%20profiles%20evaluation%20%28ICTWS%202018%29_removed.pdf
    • Vancouver

      Ribeiro ML, Almeida Júnior JHS, Garcia JDA, Tita V. Progressive failure analysis of composite cylinders under transverse impact via high order finite element formulation: through-the-thickness stress profiles evaluation [Internet]. Proceedings of CNB2019. 2018 ;[citado 2024 jun. 03 ] Available from: https://repositorio.usp.br/directbitstream/4e5aa62d-b68b-42f8-a789-28f54d186fe3/trabalho%2012%20-%20%20Progressive%20failure%20analysis%20of%20composite%20cylinders%20under%20transverse%20impact%20via%20high%20order%20finite%20element%20formulation%20through-the-thickness%20stress%20profiles%20evaluation%20%28ICTWS%202018%29_removed.pdf
  • Source: Composites Part B. Unidade: EESC

    Subjects: FLAMBAGEM, MÉTODO DOS ELEMENTOS FINITOS, ENGENHARIA AERONÁUTICA

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      ALMEIDA JÚNIOR, José Humberto Santos et al. Buckling and post-buckling of filament wound composite tubes under axial compression: linear, nonlinear, damage and experimental analyses. Composites Part B, v. 149, p. 227-239, 2018Tradução . . Disponível em: https://doi.org/10.1016/j.compositesb.2018.05.004. Acesso em: 03 jun. 2024.
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      Almeida Júnior, J. H. S., Tonatto, M. L. P., Ribeiro, M. L., Tita, V., & Amico, S. C. (2018). Buckling and post-buckling of filament wound composite tubes under axial compression: linear, nonlinear, damage and experimental analyses. Composites Part B, 149, 227-239. doi:10.1016/j.compositesb.2018.05.004
    • NLM

      Almeida Júnior JHS, Tonatto MLP, Ribeiro ML, Tita V, Amico SC. Buckling and post-buckling of filament wound composite tubes under axial compression: linear, nonlinear, damage and experimental analyses [Internet]. Composites Part B. 2018 ; 149 227-239.[citado 2024 jun. 03 ] Available from: https://doi.org/10.1016/j.compositesb.2018.05.004
    • Vancouver

      Almeida Júnior JHS, Tonatto MLP, Ribeiro ML, Tita V, Amico SC. Buckling and post-buckling of filament wound composite tubes under axial compression: linear, nonlinear, damage and experimental analyses [Internet]. Composites Part B. 2018 ; 149 227-239.[citado 2024 jun. 03 ] Available from: https://doi.org/10.1016/j.compositesb.2018.05.004
  • Source: Composite Structures. Unidade: EESC

    Subjects: MÉTODO DOS ELEMENTOS FINITOS, ALGORITMOS GENÉTICOS, MATERIAIS COMPÓSITOS, FALHA, ENGENHARIA AERONÁUTICA

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      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: 03 jun. 2024.
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      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
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      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 2024 jun. 03 ] 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 2024 jun. 03 ] Available from: https://doi.org/10.1016/j.compstruct.2017.07.054
  • Source: Composite Structures. Unidade: EESC

    Subjects: ANÁLISE NUMÉRICA, FALHA, MÉTODO DOS ELEMENTOS FINITOS

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      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: 03 jun. 2024.
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      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
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      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 2024 jun. 03 ] 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 2024 jun. 03 ] Available from: https://doi.org/10.1016/j.compstruct.2016.10.036
  • Source: Proceedings. Conference titles: Brazilian Conference on Composite Materials. Unidade: EESC

    Subjects: ALGORITMOS GENÉTICOS, MÉTODO DOS ELEMENTOS FINITOS, MATERIAIS COMPÓSITOS, ENGENHARIA AERONÁUTICA

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      ALMEIDA JÚNIOR, José Humberto Santos et al. Optimization of the stacking sequence for filament wound composite tubes under internal pressure using a genetic algorithm. 2016, Anais.. Porto Alegre, RS: UFRGS, 2016. . Acesso em: 03 jun. 2024.
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      Almeida Júnior, J. H. S., Ribeiro, M. L., Tita, V., & Amico, S. C. (2016). Optimization of the stacking sequence for filament wound composite tubes under internal pressure using a genetic algorithm. In Proceedings. Porto Alegre, RS: UFRGS.
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      Almeida Júnior JHS, Ribeiro ML, Tita V, Amico SC. Optimization of the stacking sequence for filament wound composite tubes under internal pressure using a genetic algorithm. Proceedings. 2016 ;[citado 2024 jun. 03 ]
    • Vancouver

      Almeida Júnior JHS, Ribeiro ML, Tita V, Amico SC. Optimization of the stacking sequence for filament wound composite tubes under internal pressure using a genetic algorithm. Proceedings. 2016 ;[citado 2024 jun. 03 ]
  • Source: Materials and Design. Unidade: EESC

    Subjects: MÉTODO DOS ELEMENTOS FINITOS, TUBOS, FALHA

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      ALMEIDA JÚNIOR, José Humberto Santos et al. Damage and failure in carbon/epoxy filament wound composite tubes under external pressure: experimental and numerical approaches. Materials and Design, v. 96, p. 431-438, 2016Tradução . . Disponível em: https://doi.org/10.1016/j.matdes.2016.02.054. Acesso em: 03 jun. 2024.
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      Almeida Júnior, J. H. S., Ribeiro, M. L., Tita, V., & Amico, S. C. (2016). Damage and failure in carbon/epoxy filament wound composite tubes under external pressure: experimental and numerical approaches. Materials and Design, 96, 431-438. doi:10.1016/j.matdes.2016.02.054
    • NLM

      Almeida Júnior JHS, Ribeiro ML, Tita V, Amico SC. Damage and failure in carbon/epoxy filament wound composite tubes under external pressure: experimental and numerical approaches [Internet]. Materials and Design. 2016 ; 96 431-438.[citado 2024 jun. 03 ] Available from: https://doi.org/10.1016/j.matdes.2016.02.054
    • Vancouver

      Almeida Júnior JHS, Ribeiro ML, Tita V, Amico SC. Damage and failure in carbon/epoxy filament wound composite tubes under external pressure: experimental and numerical approaches [Internet]. Materials and Design. 2016 ; 96 431-438.[citado 2024 jun. 03 ] Available from: https://doi.org/10.1016/j.matdes.2016.02.054
  • Source: Proceedings. Conference titles: International Conference on Composite Materials. Unidade: EESC

    Subjects: ESTRUTURAS MISTAS, FALHA, ENGENHARIA AERONÁUTICA

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      ALMEIDA JÚNIOR, José Humberto Santos et al. Progressive failure analysis of filament wound composite tubes under internal pressure. 2015, Anais.. Copenhagen, Denmark: ICCM, 2015. Disponível em: https://repositorio.usp.br/directbitstream/954d5c47-7cb9-4de0-8d70-cdaee476d031/trabalho%20PROGRESSIVE%20FAILURE%20ANALYSIS%20OF%20FILAMENT%20WOUND%20COMPOSITE%20TUBES%20UNDER%20INTERNAL%20PRESSURE_removed%20%281%29.pdf. Acesso em: 03 jun. 2024.
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      Almeida Júnior, J. H. S., Ribeiro, M. L., Tita, V., Faria, H., Marques, A. T., & Amico, S. C. (2015). Progressive failure analysis of filament wound composite tubes under internal pressure. In Proceedings. Copenhagen, Denmark: ICCM. Recuperado de https://repositorio.usp.br/directbitstream/954d5c47-7cb9-4de0-8d70-cdaee476d031/trabalho%20PROGRESSIVE%20FAILURE%20ANALYSIS%20OF%20FILAMENT%20WOUND%20COMPOSITE%20TUBES%20UNDER%20INTERNAL%20PRESSURE_removed%20%281%29.pdf
    • NLM

      Almeida Júnior JHS, Ribeiro ML, Tita V, Faria H, Marques AT, Amico SC. Progressive failure analysis of filament wound composite tubes under internal pressure [Internet]. Proceedings. 2015 ;[citado 2024 jun. 03 ] Available from: https://repositorio.usp.br/directbitstream/954d5c47-7cb9-4de0-8d70-cdaee476d031/trabalho%20PROGRESSIVE%20FAILURE%20ANALYSIS%20OF%20FILAMENT%20WOUND%20COMPOSITE%20TUBES%20UNDER%20INTERNAL%20PRESSURE_removed%20%281%29.pdf
    • Vancouver

      Almeida Júnior JHS, Ribeiro ML, Tita V, Faria H, Marques AT, Amico SC. Progressive failure analysis of filament wound composite tubes under internal pressure [Internet]. Proceedings. 2015 ;[citado 2024 jun. 03 ] Available from: https://repositorio.usp.br/directbitstream/954d5c47-7cb9-4de0-8d70-cdaee476d031/trabalho%20PROGRESSIVE%20FAILURE%20ANALYSIS%20OF%20FILAMENT%20WOUND%20COMPOSITE%20TUBES%20UNDER%20INTERNAL%20PRESSURE_removed%20%281%29.pdf
  • Source: Proceedings. Conference titles: International Conference on Composite Materials. Unidade: EESC

    Subjects: MÉTODO DOS ELEMENTOS FINITOS, FALHA, FLAMBAGEM, ENGENHARIA AERONÁUTICA

    How to cite
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • ABNT

      ALMEIDA JÚNIOR, José Humberto Santos et al. Buckling and post-buckling in filament wound composite tubes under transverse compression. 2015, Anais.. Copenhagen, Denmark: ICCM, 2015. . Acesso em: 03 jun. 2024.
    • APA

      Almeida Júnior, J. H. S., Ribeiro, M. L., Tita, V., Faria, H., Marques, A. T., & Amico, S. C. (2015). Buckling and post-buckling in filament wound composite tubes under transverse compression. In Proceedings. Copenhagen, Denmark: ICCM.
    • NLM

      Almeida Júnior JHS, Ribeiro ML, Tita V, Faria H, Marques AT, Amico SC. Buckling and post-buckling in filament wound composite tubes under transverse compression. Proceedings. 2015 ;[citado 2024 jun. 03 ]
    • Vancouver

      Almeida Júnior JHS, Ribeiro ML, Tita V, Faria H, Marques AT, Amico SC. Buckling and post-buckling in filament wound composite tubes under transverse compression. Proceedings. 2015 ;[citado 2024 jun. 03 ]

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