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  • Source: Proceedings of MECSOL. Conference titles: International Symposium on Solid Mechanics - MECSOL. Unidade: EESC

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

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    • ABNT

      SANTANA, Humberto Brito et al. Effective elastic properties for a periodically laminated composite considering nonuniform imperfect adhesion. 2017, Anais.. Joinville, SC: Escola de Engenharia de São Carlos, Universidade de São Paulo, 2017. . Acesso em: 23 abr. 2024.
    • APA

      Santana, H. B., Jaramillo Bustamante, L. E., Medeiros, R. de, Ribeiro, M. L., Tita, V., & Rodríguez Ramos, R. (2017). Effective elastic properties for a periodically laminated composite considering nonuniform imperfect adhesion. In Proceedings of MECSOL. Joinville, SC: Escola de Engenharia de São Carlos, Universidade de São Paulo.
    • NLM

      Santana HB, Jaramillo Bustamante LE, Medeiros R de, Ribeiro ML, Tita V, Rodríguez Ramos R. Effective elastic properties for a periodically laminated composite considering nonuniform imperfect adhesion. Proceedings of MECSOL. 2017 ;[citado 2024 abr. 23 ]
    • Vancouver

      Santana HB, Jaramillo Bustamante LE, Medeiros R de, Ribeiro ML, Tita V, Rodríguez Ramos R. Effective elastic properties for a periodically laminated composite considering nonuniform imperfect adhesion. Proceedings of MECSOL. 2017 ;[citado 2024 abr. 23 ]
  • Source: Anais. Conference titles: Meeting on Aeronautical Composite Materials and Structures - MACMS 2015. Unidade: EESC

    Subjects: BIOMATERIAIS, MATERIAIS COMPÓSITOS, ESTRUTURA DE AERONAVES, INTERIOR DE AERONAVES, ENGENHARIA AERONÁUTICA

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    • ABNT

      ELOY, Felipe de S. et al. Comparison between mechanical properties of bio and synthetic composites for use in aircraft interior structures. 2017, Anais.. São Carlos, SP: EESC-USP, 2017. Disponível em: http://soac.eesc.usp.br/index.php/macms/macms/paper/view/330/268. Acesso em: 23 abr. 2024.
    • APA

      Eloy, F. de S., Costa, R. R. C. da, Medeiros, R. de, Ribeiro, M. L., & Tita, V. (2017). Comparison between mechanical properties of bio and synthetic composites for use in aircraft interior structures. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/macms/macms/paper/view/330/268
    • NLM

      Eloy F de S, Costa RRC da, Medeiros R de, Ribeiro ML, Tita V. Comparison between mechanical properties of bio and synthetic composites for use in aircraft interior structures [Internet]. Anais. 2017 ;[citado 2024 abr. 23 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms/paper/view/330/268
    • Vancouver

      Eloy F de S, Costa RRC da, Medeiros R de, Ribeiro ML, Tita V. Comparison between mechanical properties of bio and synthetic composites for use in aircraft interior structures [Internet]. Anais. 2017 ;[citado 2024 abr. 23 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms/paper/view/330/268
  • Source: Anais. Conference titles: Meeting on Aeronautical Composite Materials and Structures - MACMS 2015. Unidade: EESC

    Subjects: DANO, MÉTODO DOS ELEMENTOS FINITOS, ENGENHARIA AERONÁUTICA

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    • ABNT

      ALMEIDA JR., José Humberto S. et al. Influence of stacking sequence on the radial compression of filament wound composite tubes. 2017, Anais.. São Carlos, SP: EESC-USP, 2017. Disponível em: http://soac.eesc.usp.br/index.php/macms/macms/paper/view/318/255. Acesso em: 23 abr. 2024.
    • APA

      Almeida Jr., J. H. S., Ribeiro, M. L., Tita, V., & Amico, S. C. (2017). Influence of stacking sequence on the radial compression of filament wound composite tubes. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/macms/macms/paper/view/318/255
    • NLM

      Almeida Jr. JHS, Ribeiro ML, Tita V, Amico SC. Influence of stacking sequence on the radial compression of filament wound composite tubes [Internet]. Anais. 2017 ;[citado 2024 abr. 23 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms/paper/view/318/255
    • Vancouver

      Almeida Jr. JHS, Ribeiro ML, Tita V, Amico SC. Influence of stacking sequence on the radial compression of filament wound composite tubes [Internet]. Anais. 2017 ;[citado 2024 abr. 23 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms/paper/view/318/255
  • Source: Anais. Conference titles: Meeting on Aeronautical Composite Materials and Structures - MACMS 2017. Unidade: EESC

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

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    • ABNT

      MADUREIRA, Fernando e RIBEIRO, Marcelo Leite. Strenght prediction of single lap joints: 3D cohesive zone modelling. 2017, Anais.. São Carlos, SP: EESC-USP, 2017. Disponível em: http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/1019/541. Acesso em: 23 abr. 2024.
    • APA

      Madureira, F., & Ribeiro, M. L. (2017). Strenght prediction of single lap joints: 3D cohesive zone modelling. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/1019/541
    • NLM

      Madureira F, Ribeiro ML. Strenght prediction of single lap joints: 3D cohesive zone modelling [Internet]. Anais. 2017 ;[citado 2024 abr. 23 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/1019/541
    • Vancouver

      Madureira F, Ribeiro ML. Strenght prediction of single lap joints: 3D cohesive zone modelling [Internet]. Anais. 2017 ;[citado 2024 abr. 23 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/1019/541
  • Conference titles: ABCM International Congress of Mechanical Engineering - COBEM. Unidade: EESC

    Subjects: MÉTODO DOS ELEMENTOS FINITOS, VIBRAÇÕES, ENGENHARIA AERONÁUTICA

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      RIBEIRO, Marcelo Leite et al. Dynamic analysis of laminate plates via carrera unified formulation. 2017, Anais.. Rio de Janeiro, RJ: ABCM, 2017. Disponível em: https://repositorio.usp.br/directbitstream/90152b7e-c9c3-43be-b3f1-f5d53dff656c/trabalho%2026%20-%20DYNAMIC%20ANALYSIS%20OF%20LAMINATE%20PLATES%20VIA%20CARRERA%20UNIFIED%20FORMULATION%20%28COBEM%202017%29_removed.pdf. Acesso em: 23 abr. 2024.
    • APA

      Ribeiro, M. L., Sartorato, M., Medeiros, R. de, Ferreira, A. J. M., & Tita, V. (2017). Dynamic analysis of laminate plates via carrera unified formulation. In . Rio de Janeiro, RJ: ABCM. Recuperado de https://repositorio.usp.br/directbitstream/90152b7e-c9c3-43be-b3f1-f5d53dff656c/trabalho%2026%20-%20DYNAMIC%20ANALYSIS%20OF%20LAMINATE%20PLATES%20VIA%20CARRERA%20UNIFIED%20FORMULATION%20%28COBEM%202017%29_removed.pdf
    • NLM

      Ribeiro ML, Sartorato M, Medeiros R de, Ferreira AJM, Tita V. Dynamic analysis of laminate plates via carrera unified formulation [Internet]. 2017 ;[citado 2024 abr. 23 ] Available from: https://repositorio.usp.br/directbitstream/90152b7e-c9c3-43be-b3f1-f5d53dff656c/trabalho%2026%20-%20DYNAMIC%20ANALYSIS%20OF%20LAMINATE%20PLATES%20VIA%20CARRERA%20UNIFIED%20FORMULATION%20%28COBEM%202017%29_removed.pdf
    • Vancouver

      Ribeiro ML, Sartorato M, Medeiros R de, Ferreira AJM, Tita V. Dynamic analysis of laminate plates via carrera unified formulation [Internet]. 2017 ;[citado 2024 abr. 23 ] Available from: https://repositorio.usp.br/directbitstream/90152b7e-c9c3-43be-b3f1-f5d53dff656c/trabalho%2026%20-%20DYNAMIC%20ANALYSIS%20OF%20LAMINATE%20PLATES%20VIA%20CARRERA%20UNIFIED%20FORMULATION%20%28COBEM%202017%29_removed.pdf
  • Source: Proceedings. Conference titles: Brazilian Conference on Composite Materials. Unidade: EESC

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

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      GARCIA, David A e TITA, Volnei e RIBEIRO, Marcelo Leite. A finite element damage model to predict failure behavior of composite sandwich structures. 2016, Anais.. Porto Alegre, RS: UFRGS, 2016. . Acesso em: 23 abr. 2024.
    • APA

      Garcia, D. A., Tita, V., & Ribeiro, M. L. (2016). A finite element damage model to predict failure behavior of composite sandwich structures. In Proceedings. Porto Alegre, RS: UFRGS.
    • NLM

      Garcia DA, Tita V, Ribeiro ML. A finite element damage model to predict failure behavior of composite sandwich structures. Proceedings. 2016 ;[citado 2024 abr. 23 ]
    • Vancouver

      Garcia DA, Tita V, Ribeiro ML. A finite element damage model to predict failure behavior of composite sandwich structures. Proceedings. 2016 ;[citado 2024 abr. 23 ]
  • Source: Proceedings. Conference titles: Brazilian Conference on Composite Materials. Unidade: EESC

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

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      MEDEIROS, Ricardo de et al. Computational analysis of residual flexural properties on composite plates. 2016, Anais.. Porto Alegre, RS: UFRGS, 2016. . Acesso em: 23 abr. 2024.
    • APA

      Medeiros, R. de, Ribeiro, M. L., Vandepitte, D., & Tita, V. (2016). Computational analysis of residual flexural properties on composite plates. In Proceedings. Porto Alegre, RS: UFRGS.
    • NLM

      Medeiros R de, Ribeiro ML, Vandepitte D, Tita V. Computational analysis of residual flexural properties on composite plates. Proceedings. 2016 ;[citado 2024 abr. 23 ]
    • Vancouver

      Medeiros R de, Ribeiro ML, Vandepitte D, Tita V. Computational analysis of residual flexural properties on composite plates. Proceedings. 2016 ;[citado 2024 abr. 23 ]
  • Source: Anais. Conference titles: Simpósio do Programa de Pós-Graduação em Engenharia Mecânica - SIPGEM. Unidade: EESC

    Subjects: MATERIAIS COMPÓSITOS, ENGENHARIA MECÂNICA

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      SANTOS, Matheus Vilar Mota et al. Carbon-fibre/epoxy laminated plate: evaluation of residual flexural properties after delamination failure. 2016, Anais.. São Carlos, SP: EESC-USP, 2016. Disponível em: http://soac.eesc.usp.br/index.php/SiPGEM/SiPGEM/paper/view/120/67. Acesso em: 23 abr. 2024.
    • APA

      Santos, M. V. M., Aveiga, D., Ferreira, G. F. O., & Ribeiro, M. L. (2016). Carbon-fibre/epoxy laminated plate: evaluation of residual flexural properties after delamination failure. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/SiPGEM/SiPGEM/paper/view/120/67
    • NLM

      Santos MVM, Aveiga D, Ferreira GFO, Ribeiro ML. Carbon-fibre/epoxy laminated plate: evaluation of residual flexural properties after delamination failure [Internet]. Anais. 2016 ;[citado 2024 abr. 23 ] Available from: http://soac.eesc.usp.br/index.php/SiPGEM/SiPGEM/paper/view/120/67
    • Vancouver

      Santos MVM, Aveiga D, Ferreira GFO, Ribeiro ML. Carbon-fibre/epoxy laminated plate: evaluation of residual flexural properties after delamination failure [Internet]. Anais. 2016 ;[citado 2024 abr. 23 ] Available from: http://soac.eesc.usp.br/index.php/SiPGEM/SiPGEM/paper/view/120/67
  • 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: 23 abr. 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 abr. 23 ]
    • 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 abr. 23 ]
  • 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: 23 abr. 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 abr. 23 ] 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 abr. 23 ] Available from: https://doi.org/10.1016/j.matdes.2016.02.054
  • Source: Anais. Conference titles: Simpósio do Programa de Pós-Graduação em Engenharia Mecânica - SIPGEM. Unidade: EESC

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

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      MADUREIRA, Fernando e RIBEIRO, Marcelo Leite. Análise numérica de juntas duplas coladas: reforço de fibra de vidro com matriz de PU de óleo de mamona e reforço de fibra vidro com matriz epóxi. 2016, Anais.. São Carlos, SP: EESC-USP, 2016. Disponível em: http://soac.eesc.usp.br/index.php/SiPGEM/SiPGEM/paper/view/129/56. Acesso em: 23 abr. 2024.
    • APA

      Madureira, F., & Ribeiro, M. L. (2016). Análise numérica de juntas duplas coladas: reforço de fibra de vidro com matriz de PU de óleo de mamona e reforço de fibra vidro com matriz epóxi. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/SiPGEM/SiPGEM/paper/view/129/56
    • NLM

      Madureira F, Ribeiro ML. Análise numérica de juntas duplas coladas: reforço de fibra de vidro com matriz de PU de óleo de mamona e reforço de fibra vidro com matriz epóxi [Internet]. Anais. 2016 ;[citado 2024 abr. 23 ] Available from: http://soac.eesc.usp.br/index.php/SiPGEM/SiPGEM/paper/view/129/56
    • Vancouver

      Madureira F, Ribeiro ML. Análise numérica de juntas duplas coladas: reforço de fibra de vidro com matriz de PU de óleo de mamona e reforço de fibra vidro com matriz epóxi [Internet]. Anais. 2016 ;[citado 2024 abr. 23 ] Available from: http://soac.eesc.usp.br/index.php/SiPGEM/SiPGEM/paper/view/129/56
  • Source: Journal of Mineral Metal and Material Engineering. Unidade: EESC

    Subjects: JUNTAS APARAFUSADAS, MATERIAIS COMPÓSITOS

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      MEDEIROS, Ricardo de e RIBEIRO, Marcelo Leite e TITA, Volnei. Experimental methodology for testing metal-composite bolted joints. Journal of Mineral Metal and Material Engineering, v. 2, p. 11-22, 2016Tradução . . Disponível em: http://www.synchropublisher.com/jms/index.php/JMMME/article/view/78. Acesso em: 23 abr. 2024.
    • APA

      Medeiros, R. de, Ribeiro, M. L., & Tita, V. (2016). Experimental methodology for testing metal-composite bolted joints. Journal of Mineral Metal and Material Engineering, 2, 11-22. Recuperado de http://www.synchropublisher.com/jms/index.php/JMMME/article/view/78
    • NLM

      Medeiros R de, Ribeiro ML, Tita V. Experimental methodology for testing metal-composite bolted joints [Internet]. Journal of Mineral Metal and Material Engineering. 2016 ; 2 11-22.[citado 2024 abr. 23 ] Available from: http://www.synchropublisher.com/jms/index.php/JMMME/article/view/78
    • Vancouver

      Medeiros R de, Ribeiro ML, Tita V. Experimental methodology for testing metal-composite bolted joints [Internet]. Journal of Mineral Metal and Material Engineering. 2016 ; 2 11-22.[citado 2024 abr. 23 ] Available from: http://www.synchropublisher.com/jms/index.php/JMMME/article/view/78
  • 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: 23 abr. 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 abr. 23 ] 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 abr. 23 ] 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: Anais. Conference titles: International Congress of Mechanical Engineering - COBEM. Unidade: EESC

    Subjects: MATERIAIS COMPÓSITOS, LAMINADOS, AERONAVES, ENGENHARIA AERONÁUTICA

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      MEDEIROS, Ricardo de et al. Residual strength criterion based on damage metric and flexural after impact (FAI) test for composite materials. 2015, Anais.. Rio de Janeiro, RJ: ABCM, 2015. . Acesso em: 23 abr. 2024.
    • APA

      Medeiros, R. de, Sartorato, M., Tita, S. P. da S., Vandepitte, D., Ribeiro, M. L., & Tita, V. (2015). Residual strength criterion based on damage metric and flexural after impact (FAI) test for composite materials. In Anais. Rio de Janeiro, RJ: ABCM.
    • NLM

      Medeiros R de, Sartorato M, Tita SP da S, Vandepitte D, Ribeiro ML, Tita V. Residual strength criterion based on damage metric and flexural after impact (FAI) test for composite materials. Anais. 2015 ;[citado 2024 abr. 23 ]
    • Vancouver

      Medeiros R de, Sartorato M, Tita SP da S, Vandepitte D, Ribeiro ML, Tita V. Residual strength criterion based on damage metric and flexural after impact (FAI) test for composite materials. Anais. 2015 ;[citado 2024 abr. 23 ]
  • Source: Anais. Conference titles: Meeting on Aeronautical Composite Materials and Structures - MACMS 2015. Unidade: EESC

    Subjects: PLÁSTICOS REFORÇADOS COM FIBRAS, RESISTÊNCIA A TRAÇÃO, ENGENHARIA AERONÁUTICA

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      VIEIRA, André Ferreira Costa et al. Loading rate effect on the tensile properties of glass fiber reinforced castor oil polyurethane and epoxy resins. 2015, Anais.. São Carlos, SP: EESC-USP, 2015. Disponível em: https://repositorio.usp.br/directbitstream/afcc4dc4-2f11-4650-baea-26f5ad2ea56b/TRABALHO%2039%20-%20Loading%20rate%20effect%20on%20the%20tensile%20properties%20of%20glass%20fiber%20reinforced%20castor%20oil%20polyurethane%20and%20epoxy%20resins%20%28macms%202015%29_removed.pdf. Acesso em: 23 abr. 2024.
    • APA

      Vieira, A. F. C., Cavalcante, R. R., Ribeiro, M. L., & Tita, V. (2015). Loading rate effect on the tensile properties of glass fiber reinforced castor oil polyurethane and epoxy resins. In Anais. São Carlos, SP: EESC-USP. Recuperado de https://repositorio.usp.br/directbitstream/afcc4dc4-2f11-4650-baea-26f5ad2ea56b/TRABALHO%2039%20-%20Loading%20rate%20effect%20on%20the%20tensile%20properties%20of%20glass%20fiber%20reinforced%20castor%20oil%20polyurethane%20and%20epoxy%20resins%20%28macms%202015%29_removed.pdf
    • NLM

      Vieira AFC, Cavalcante RR, Ribeiro ML, Tita V. Loading rate effect on the tensile properties of glass fiber reinforced castor oil polyurethane and epoxy resins [Internet]. Anais. 2015 ;[citado 2024 abr. 23 ] Available from: https://repositorio.usp.br/directbitstream/afcc4dc4-2f11-4650-baea-26f5ad2ea56b/TRABALHO%2039%20-%20Loading%20rate%20effect%20on%20the%20tensile%20properties%20of%20glass%20fiber%20reinforced%20castor%20oil%20polyurethane%20and%20epoxy%20resins%20%28macms%202015%29_removed.pdf
    • Vancouver

      Vieira AFC, Cavalcante RR, Ribeiro ML, Tita V. Loading rate effect on the tensile properties of glass fiber reinforced castor oil polyurethane and epoxy resins [Internet]. Anais. 2015 ;[citado 2024 abr. 23 ] Available from: https://repositorio.usp.br/directbitstream/afcc4dc4-2f11-4650-baea-26f5ad2ea56b/TRABALHO%2039%20-%20Loading%20rate%20effect%20on%20the%20tensile%20properties%20of%20glass%20fiber%20reinforced%20castor%20oil%20polyurethane%20and%20epoxy%20resins%20%28macms%202015%29_removed.pdf
  • Source: International Journal of Automotive Composites. Unidade: EESC

    Subjects: ESTRUTURAS MISTAS, DANO, MÉTODO DOS ELEMENTOS FINITOS

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      RIBEIRO, Marcelo Leite e MEDEIROS, Ricardo de. Computational parametric study of low-velocity impact response of composite cylinder for automotive components. International Journal of Automotive Composites, v. 1, n. 1, p. 112-128, 2015Tradução . . Disponível em: https://repositorio.usp.br/directbitstream/8e02362c-ec63-4436-b3ef-50c112122143/artigo%2015%20-%20Computational%20parametric%20study%20of%20low-velocity%20impact%20response%20of%20composite%20cylinder%20for%20automotive%20components%20%28International%20Journal%20of%20Automotive%20Composites%29.pdf. Acesso em: 23 abr. 2024.
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      Ribeiro, M. L., & Medeiros, R. de. (2015). Computational parametric study of low-velocity impact response of composite cylinder for automotive components. International Journal of Automotive Composites, 1( 1), 112-128. Recuperado de https://repositorio.usp.br/directbitstream/8e02362c-ec63-4436-b3ef-50c112122143/artigo%2015%20-%20Computational%20parametric%20study%20of%20low-velocity%20impact%20response%20of%20composite%20cylinder%20for%20automotive%20components%20%28International%20Journal%20of%20Automotive%20Composites%29.pdf
    • NLM

      Ribeiro ML, Medeiros R de. Computational parametric study of low-velocity impact response of composite cylinder for automotive components [Internet]. International Journal of Automotive Composites. 2015 ; 1( 1): 112-128.[citado 2024 abr. 23 ] Available from: https://repositorio.usp.br/directbitstream/8e02362c-ec63-4436-b3ef-50c112122143/artigo%2015%20-%20Computational%20parametric%20study%20of%20low-velocity%20impact%20response%20of%20composite%20cylinder%20for%20automotive%20components%20%28International%20Journal%20of%20Automotive%20Composites%29.pdf
    • Vancouver

      Ribeiro ML, Medeiros R de. Computational parametric study of low-velocity impact response of composite cylinder for automotive components [Internet]. International Journal of Automotive Composites. 2015 ; 1( 1): 112-128.[citado 2024 abr. 23 ] Available from: https://repositorio.usp.br/directbitstream/8e02362c-ec63-4436-b3ef-50c112122143/artigo%2015%20-%20Computational%20parametric%20study%20of%20low-velocity%20impact%20response%20of%20composite%20cylinder%20for%20automotive%20components%20%28International%20Journal%20of%20Automotive%20Composites%29.pdf
  • Source: Proceedings. Conference titles: International Conference on Composite Materials. Unidade: EESC

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

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      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: 23 abr. 2024.
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      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 abr. 23 ]
    • 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 abr. 23 ]
  • Source: Anais. Conference titles: International Congress of Mechanical Engineering - COBEM. Unidade: EESC

    Subjects: HOMOGENEIZAÇÃO, CISALHAMENTO, LAMINADOS, ENGENHARIA AERONÁUTICA

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      SANTANA, Humberto Brito et al. A dispersive nonlocal model for shear wave propagation in a periodically perfect/imperfect connected multi-laminated. 2015, Anais.. Rio de Janeiro, RJ: ABCM, 2015. . Acesso em: 23 abr. 2024.
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      Santana, H. B., Tita, V., Ribeiro, M. L., Rodríguez Ramos, R., Bravo Castillero, J., & Guinovart-Díaz, R. (2015). A dispersive nonlocal model for shear wave propagation in a periodically perfect/imperfect connected multi-laminated. In Anais. Rio de Janeiro, RJ: ABCM.
    • NLM

      Santana HB, Tita V, Ribeiro ML, Rodríguez Ramos R, Bravo Castillero J, Guinovart-Díaz R. A dispersive nonlocal model for shear wave propagation in a periodically perfect/imperfect connected multi-laminated. Anais. 2015 ;[citado 2024 abr. 23 ]
    • Vancouver

      Santana HB, Tita V, Ribeiro ML, Rodríguez Ramos R, Bravo Castillero J, Guinovart-Díaz R. A dispersive nonlocal model for shear wave propagation in a periodically perfect/imperfect connected multi-laminated. Anais. 2015 ;[citado 2024 abr. 23 ]
  • Source: Composite Structures. Unidade: EESC

    Subjects: ANÁLISE EXPERIMENTAL DE ESTRUTURAS, DANO, ESTRUTURAS (IMPACTO)

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      RIBEIRO, Marcelo Leite e VANDEPITTE, Dirk e TITA, Volnei. Experimental analysis of transverse impact loading on composite cylinders. Composite Structures, v. 133, p. 547-563, 2015Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2015.07.088. Acesso em: 23 abr. 2024.
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      Ribeiro, M. L., Vandepitte, D., & Tita, V. (2015). Experimental analysis of transverse impact loading on composite cylinders. Composite Structures, 133, 547-563. doi:10.1016/j.compstruct.2015.07.088
    • NLM

      Ribeiro ML, Vandepitte D, Tita V. Experimental analysis of transverse impact loading on composite cylinders [Internet]. Composite Structures. 2015 ; 133 547-563.[citado 2024 abr. 23 ] Available from: https://doi.org/10.1016/j.compstruct.2015.07.088
    • Vancouver

      Ribeiro ML, Vandepitte D, Tita V. Experimental analysis of transverse impact loading on composite cylinders [Internet]. Composite Structures. 2015 ; 133 547-563.[citado 2024 abr. 23 ] Available from: https://doi.org/10.1016/j.compstruct.2015.07.088
  • Source: Anais. Conference titles: International Congress of Mechanical Engineering - COBEM. Unidade: EESC

    Subjects: FADIGA DE AERONAVES, MATERIAIS COMPÓSITOS, LAMINADOS, ENGENHARIA AERONÁUTICA

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      MEDEIROS, Ricardo de et al. Computational tool for fatigue analysis in composite material. 2015, Anais.. Rio de Janeiro, RJ: ABCM, 2015. . Acesso em: 23 abr. 2024.
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      Medeiros, R. de, Daniel, G. S., Ribeiro, M. L., & Tita, V. (2015). Computational tool for fatigue analysis in composite material. In Anais. Rio de Janeiro, RJ: ABCM.
    • NLM

      Medeiros R de, Daniel GS, Ribeiro ML, Tita V. Computational tool for fatigue analysis in composite material. Anais. 2015 ;[citado 2024 abr. 23 ]
    • Vancouver

      Medeiros R de, Daniel GS, Ribeiro ML, Tita V. Computational tool for fatigue analysis in composite material. Anais. 2015 ;[citado 2024 abr. 23 ]

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