Filtros : "Almeida Júnior, José Humberto Santos" Removido: "Bittrich, Lars" Limpar

Filtros



Limitar por data


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

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

    Versão PublicadaAcesso à fonteDOIComo citar
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • ABNT

      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: 01 out. 2024.
    • APA

      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 out. 01 ] 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 out. 01 ] Available from: https://dx.doi.org/10.1016/j.tafmec.2024.104424
  • Fonte: Composites Science and Technology. Unidade: EESC

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

    Versão PublicadaAcesso à fonteDOIComo citar
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • ABNT

      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: 01 out. 2024.
    • APA

      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
    • NLM

      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 out. 01 ] 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 out. 01 ] Available from: https://doi.org/10.1016/j.compscitech.2022.109872
  • Fonte: Engineering Structures. Unidade: EESC

    Assuntos: TOPOLOGIA, HOMOGENEIZAÇÃO, ENGENHARIA AERONÁUTICA

    Versão PublicadaAcesso à fonteDOIComo citar
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • ABNT

      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: 01 out. 2024.
    • APA

      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 out. 01 ] 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 out. 01 ] Available from: https://doi.org/10.1016/j.engstruct.2023.115990
  • Fonte: Thin-Walled Structures. Unidade: EESC

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

    PrivadoAcesso à fonteDOIComo citar
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • ABNT

      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: 01 out. 2024.
    • APA

      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 out. 01 ] 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 out. 01 ] Available from: https://doi.org/10.1016/j.tws.2021.108864
  • Fonte: Composites Part B. Unidade: EESC

    Assuntos: PROCESSOS DE FABRICAÇÃO, FLAMBAGEM, ENGENHARIA AERONÁUTICA

    PrivadoAcesso à fonteDOIComo citar
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • ABNT

      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: 01 out. 2024.
    • APA

      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 out. 01 ] 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 out. 01 ] Available from: https://doi.org/10.1016/j.compositesb.2021.109224
  • Fonte: Proceedings of BCCM 5. Nome do evento: Brazilian Conference on Composite Materials - BCCM. Unidade: EESC

    Assuntos: MATERIAIS COMPÓSITOS, MÉTODO DOS ELEMENTOS FINITOS

    Versão PublicadaComo citar
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • ABNT

      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: 01 out. 2024.
    • APA

      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
    • NLM

      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 out. 01 ] 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 out. 01 ] Available from: https://repositorio.usp.br/directbitstream/0c8ccce2-ca31-481a-b1b9-7f62c1a18f56/2929-8022-1-PB.pdf
  • Fonte: Thin-Walled Structures. Unidade: EESC

    Assuntos: MÉTODO DOS ELEMENTOS FINITOS, LAMINADOS, AERONÁUTICA

    PrivadoAcesso à fonteDOIComo citar
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • ABNT

      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: 01 out. 2024.
    • APA

      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
    • NLM

      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 out. 01 ] 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 out. 01 ] Available from: https://doi.org/10.1016/j.tws.2020.107107
  • Fonte: Proceedings of CNB2019. Nome do evento: International Conference on Thin-Walled Structures - ICTWS. Unidade: EESC

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

    PrivadoComo citar
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • ABNT

      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: 01 out. 2024.
    • APA

      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
    • NLM

      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 out. 01 ] 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 out. 01 ] 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
  • Fonte: Composites Part B. Unidade: EESC

    Assuntos: FLAMBAGEM, MÉTODO DOS ELEMENTOS FINITOS, ENGENHARIA AERONÁUTICA

    PrivadoAcesso à fonteDOIComo citar
    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 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: 01 out. 2024.
    • APA

      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 out. 01 ] 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 out. 01 ] Available from: https://doi.org/10.1016/j.compositesb.2018.05.004
  • Fonte: Composite Structures. Unidade: EESC

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

    Acesso à fonteDOIComo citar
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • 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: 01 out. 2024.
    • 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 2024 out. 01 ] 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 out. 01 ] Available from: https://doi.org/10.1016/j.compstruct.2017.07.054
  • Fonte: Composite Structures. Unidade: EESC

    Assuntos: ANÁLISE NUMÉRICA, FALHA, MÉTODO DOS ELEMENTOS FINITOS

    Acesso à fonteDOIComo citar
    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: 01 out. 2024.
    • 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 2024 out. 01 ] 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 out. 01 ] Available from: https://doi.org/10.1016/j.compstruct.2016.10.036
  • Fonte: Proceedings. Nome do evento: Brazilian Conference on Composite Materials. Unidade: EESC

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

    Como citar
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • ABNT

      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: 01 out. 2024.
    • APA

      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.
    • NLM

      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 out. 01 ]
    • 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 out. 01 ]
  • Fonte: Materials and Design. Unidade: EESC

    Assuntos: MÉTODO DOS ELEMENTOS FINITOS, TUBOS, FALHA

    Acesso à fonteDOIComo citar
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • ABNT

      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: 01 out. 2024.
    • APA

      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 out. 01 ] 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 out. 01 ] Available from: https://doi.org/10.1016/j.matdes.2016.02.054
  • Fonte: Proceedings. Nome do evento: International Conference on Composite Materials. Unidade: EESC

    Assuntos: ESTRUTURAS MISTAS, FALHA, ENGENHARIA AERONÁUTICA

    PrivadoComo citar
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • ABNT

      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: 01 out. 2024.
    • APA

      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 out. 01 ] 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 out. 01 ] 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
  • Fonte: Proceedings. Nome do evento: International Conference on Composite Materials. Unidade: EESC

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

    Como citar
    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: 01 out. 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 out. 01 ]
    • 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 out. 01 ]

Biblioteca Digital de Produção Intelectual da Universidade de São Paulo     2012 - 2024