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  • Source: Composite Structures. Unidade: EESC

    Assunto: ENGENHARIA AERONÁUTICA

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    • ABNT

      SANTANA, Pedro Bührer et al. On the influence of material property uncertainties for a phenomenological progressive damage in composite laminated coupons: a sensitivity analysis approach. Composite Structures, v. 366, p. 1-15, 2025Tradução . . Disponível em: http://dx.doi.org/10.1016/j.compstruct.2025.119209. Acesso em: 17 nov. 2025.
    • APA

      Santana, P. B., Gomes, H. M., Ferreira, A. J. M., & Tita, V. (2025). On the influence of material property uncertainties for a phenomenological progressive damage in composite laminated coupons: a sensitivity analysis approach. Composite Structures, 366, 1-15. doi:10.1016/j.compstruct.2025.119209
    • NLM

      Santana PB, Gomes HM, Ferreira AJM, Tita V. On the influence of material property uncertainties for a phenomenological progressive damage in composite laminated coupons: a sensitivity analysis approach [Internet]. Composite Structures. 2025 ; 366 1-15.[citado 2025 nov. 17 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2025.119209
    • Vancouver

      Santana PB, Gomes HM, Ferreira AJM, Tita V. On the influence of material property uncertainties for a phenomenological progressive damage in composite laminated coupons: a sensitivity analysis approach [Internet]. Composite Structures. 2025 ; 366 1-15.[citado 2025 nov. 17 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2025.119209
  • Source: Composite Structures. Unidade: EESC

    Assunto: ENGENHARIA AERONÁUTICA

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    • ABNT

      ZANETTI, Matteo et al. Analysing the influence of delamination on composite structures using modal analysis and statistical indices. Composite Structures, v. 371, p. 1-17, 2025Tradução . . Disponível em: http://dx.doi.org/10.1016/j.compstruct.2025.119427. Acesso em: 17 nov. 2025.
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      Zanetti, M., Negri, D., Vandepitte, D., Tita, V., & Medeiros, R. de. (2025). Analysing the influence of delamination on composite structures using modal analysis and statistical indices. Composite Structures, 371, 1-17. doi:10.1016/j.compstruct.2025.119427
    • NLM

      Zanetti M, Negri D, Vandepitte D, Tita V, Medeiros R de. Analysing the influence of delamination on composite structures using modal analysis and statistical indices [Internet]. Composite Structures. 2025 ; 371 1-17.[citado 2025 nov. 17 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2025.119427
    • Vancouver

      Zanetti M, Negri D, Vandepitte D, Tita V, Medeiros R de. Analysing the influence of delamination on composite structures using modal analysis and statistical indices [Internet]. Composite Structures. 2025 ; 371 1-17.[citado 2025 nov. 17 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2025.119427
  • Source: Composite Structures. Unidade: EESC

    Assunto: ESTRUTURAS

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    • ABNT

      SOUZA, Vinicius de Barros e FANTUZZI, Nicholas e CODA, Humberto Breves. A smoothed Zig-Zag plate finite element for the analysis of laminated composite plates. Composite Structures, v. 371, p. 1-25, 2025Tradução . . Disponível em: http://dx.doi.org/10.1016/j.compstruct.2025.119412. Acesso em: 17 nov. 2025.
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      Souza, V. de B., Fantuzzi, N., & Coda, H. B. (2025). A smoothed Zig-Zag plate finite element for the analysis of laminated composite plates. Composite Structures, 371, 1-25. doi:10.1016/j.compstruct.2025.119412
    • NLM

      Souza V de B, Fantuzzi N, Coda HB. A smoothed Zig-Zag plate finite element for the analysis of laminated composite plates [Internet]. Composite Structures. 2025 ; 371 1-25.[citado 2025 nov. 17 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2025.119412
    • Vancouver

      Souza V de B, Fantuzzi N, Coda HB. A smoothed Zig-Zag plate finite element for the analysis of laminated composite plates [Internet]. Composite Structures. 2025 ; 371 1-25.[citado 2025 nov. 17 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2025.119412
  • Source: Composite Structures. Unidade: EESC

    Assunto: ENGENHARIA AERONÁUTICA

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      SOUZA, Gabriel Sales Candido et al. Radial compression of thin-walled variable-angle tow filament-wound composite cylinders, Part I: Manufacture, experimental, and computational analyses in the linear-elastic regime. Composite Structures, v. 366, p. 1-12, 2025Tradução . . Disponível em: http://dx.doi.org/10.1016/j.compstruct.2025.119178. Acesso em: 17 nov. 2025.
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      Souza, G. S. C., Santos, A. L. dos, Maciel, M. M. Á. D., Guedes, R. M., Viriato, N., Amico, S. C., & Tita, V. (2025). Radial compression of thin-walled variable-angle tow filament-wound composite cylinders, Part I: Manufacture, experimental, and computational analyses in the linear-elastic regime. Composite Structures, 366, 1-12. doi:10.1016/j.compstruct.2025.119178
    • NLM

      Souza GSC, Santos AL dos, Maciel MMÁD, Guedes RM, Viriato N, Amico SC, Tita V. Radial compression of thin-walled variable-angle tow filament-wound composite cylinders, Part I: Manufacture, experimental, and computational analyses in the linear-elastic regime [Internet]. Composite Structures. 2025 ; 366 1-12.[citado 2025 nov. 17 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2025.119178
    • Vancouver

      Souza GSC, Santos AL dos, Maciel MMÁD, Guedes RM, Viriato N, Amico SC, Tita V. Radial compression of thin-walled variable-angle tow filament-wound composite cylinders, Part I: Manufacture, experimental, and computational analyses in the linear-elastic regime [Internet]. Composite Structures. 2025 ; 366 1-12.[citado 2025 nov. 17 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2025.119178
  • Source: Composite Structures. Unidade: EESC

    Subjects: PIEZOELETRICIDADE, MÉTODO DOS ELEMENTOS FINITOS, ATUADORES PIEZELÉTRICOS, ENGENHARIA AERONÁUTICA

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      LONGO, Janice et al. Development of a numerical and analytical methodology for analyzing hybrid laminates with multi-oriented piezoelectric and structural layers. Composite Structures, v. 349-350, p. 1-9, 2024Tradução . . Disponível em: http://dx.doi.org/10.1016/j.compstruct.2024.118506. Acesso em: 17 nov. 2025.
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      Longo, J., Silva, M. R., Santana, H. B., Ferreira, A. J. M., Tita, V., & Medeiros, R. de. (2024). Development of a numerical and analytical methodology for analyzing hybrid laminates with multi-oriented piezoelectric and structural layers. Composite Structures, 349-350, 1-9. doi:10.1016/j.compstruct.2024.118506
    • NLM

      Longo J, Silva MR, Santana HB, Ferreira AJM, Tita V, Medeiros R de. Development of a numerical and analytical methodology for analyzing hybrid laminates with multi-oriented piezoelectric and structural layers [Internet]. Composite Structures. 2024 ; 349-350 1-9.[citado 2025 nov. 17 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2024.118506
    • Vancouver

      Longo J, Silva MR, Santana HB, Ferreira AJM, Tita V, Medeiros R de. Development of a numerical and analytical methodology for analyzing hybrid laminates with multi-oriented piezoelectric and structural layers [Internet]. Composite Structures. 2024 ; 349-350 1-9.[citado 2025 nov. 17 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2024.118506
  • Source: Composite Structures. Unidade: EESC

    Subjects: MÉTODO DOS ELEMENTOS FINITOS, ANÁLISE NÃO LINEAR DE ESTRUTURAS, DANO, ENGENHARIA AERONÁUTICA

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      SANTANA, Pedro Bührer et al. Nonlinear finite element damage analysis of laminated shells by Carrera Unified Formulation. Composite Structures, v. 348, p. 1-16, 2024Tradução . . Disponível em: http://dx.doi.org/10.1016/j.compstruct.2024.118506. Acesso em: 17 nov. 2025.
    • APA

      Santana, P. B., Ferreira, A. J. M., Gomes, H. M., & Tita, V. (2024). Nonlinear finite element damage analysis of laminated shells by Carrera Unified Formulation. Composite Structures, 348, 1-16. doi:10.1016/j.compstruct.2024.118494
    • NLM

      Santana PB, Ferreira AJM, Gomes HM, Tita V. Nonlinear finite element damage analysis of laminated shells by Carrera Unified Formulation [Internet]. Composite Structures. 2024 ; 348 1-16.[citado 2025 nov. 17 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2024.118506
    • Vancouver

      Santana PB, Ferreira AJM, Gomes HM, Tita V. Nonlinear finite element damage analysis of laminated shells by Carrera Unified Formulation [Internet]. Composite Structures. 2024 ; 348 1-16.[citado 2025 nov. 17 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2024.118506
  • Source: Composite Structures. Unidade: EP

    Subjects: CONCRETO REFORÇADO COM FIBRAS, VIGAS

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      TRINDADE, Yasmin Teixeira et al. Design of SFRC members aided by a multiscale model: part I – predicting the post-cracking parameters. Composite Structures, v. 241, p. com 14 , 2020Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2020.112078. Acesso em: 17 nov. 2025.
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      Trindade, Y. T., Bitencourt Júnior, L. A. G., Monte, R., Figueiredo, A. D. de, & Manzoli, O. L. (2020). Design of SFRC members aided by a multiscale model: part I – predicting the post-cracking parameters. Composite Structures, 241, com 14 . doi:10.1016/j.compstruct.2020.112078
    • NLM

      Trindade YT, Bitencourt Júnior LAG, Monte R, Figueiredo AD de, Manzoli OL. Design of SFRC members aided by a multiscale model: part I – predicting the post-cracking parameters [Internet]. Composite Structures. 2020 ; 241 com 14 .[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2020.112078
    • Vancouver

      Trindade YT, Bitencourt Júnior LAG, Monte R, Figueiredo AD de, Manzoli OL. Design of SFRC members aided by a multiscale model: part I – predicting the post-cracking parameters [Internet]. Composite Structures. 2020 ; 241 com 14 .[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2020.112078
  • Source: Composite Structures. Unidade: EP

    Assunto: MATERIAIS COMPÓSITOS DE FIBRAS

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      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.
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      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
  • Source: Composite Structures. Unidade: EP

    Subjects: TOPOLOGIA, TENSÃO DOS MATERIAIS, TENSOESTRUTURAS

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      KIYONO, César Yukishigue et al. A new multi-p-norm formulation approach for stress-based topology optimization design. Composite Structures, v. no 2016, p. 10-19, 2016Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2016.05.058. Acesso em: 17 nov. 2025.
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      Kiyono, C. Y., Vatanabe, S. L., Silva, E. C. N., & Reddy, J. N. (2016). A new multi-p-norm formulation approach for stress-based topology optimization design. Composite Structures, no 2016, 10-19. doi:10.1016/j.compstruct.2016.05.058
    • NLM

      Kiyono CY, Vatanabe SL, Silva ECN, Reddy JN. A new multi-p-norm formulation approach for stress-based topology optimization design [Internet]. Composite Structures. 2016 ; no 2016 10-19.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2016.05.058
    • Vancouver

      Kiyono CY, Vatanabe SL, Silva ECN, Reddy JN. A new multi-p-norm formulation approach for stress-based topology optimization design [Internet]. Composite Structures. 2016 ; no 2016 10-19.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2016.05.058

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