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  • Source: Composite Structures. Unidade: EESC

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

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    • ABNT

      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: 04 nov. 2024.
    • APA

      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 2024 nov. 04 ] 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 2024 nov. 04 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2024.118506
  • Source: Composites Part C: Open Access. Unidade: EESC

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

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    • ABNT

      SANTANA, Pedro Bührer et al. A nonlinear finite element analysis of laminated shells with a damage model. Composites Part C: Open Access, v. 15, p. 1-14, 2024Tradução . . Disponível em: http://dx.doi.org/10.1016/j.jcomc.2024.100505. Acesso em: 04 nov. 2024.
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      Santana, P. B., Ferreira, A. J. M., Gomes, H. M., & Tita, V. (2024). A nonlinear finite element analysis of laminated shells with a damage model. Composites Part C: Open Access, 15, 1-14. doi:10.1016/j.jcomc.2024.100505
    • NLM

      Santana PB, Ferreira AJM, Gomes HM, Tita V. A nonlinear finite element analysis of laminated shells with a damage model [Internet]. Composites Part C: Open Access. 2024 ; 15 1-14.[citado 2024 nov. 04 ] Available from: http://dx.doi.org/10.1016/j.jcomc.2024.100505
    • Vancouver

      Santana PB, Ferreira AJM, Gomes HM, Tita V. A nonlinear finite element analysis of laminated shells with a damage model [Internet]. Composites Part C: Open Access. 2024 ; 15 1-14.[citado 2024 nov. 04 ] Available from: http://dx.doi.org/10.1016/j.jcomc.2024.100505
  • Source: Mechanical Systems and Signal Processing. Unidade: EESC

    Subjects: POTENCIAL ELÉTRICO, SENSOR, BATERIAS ELÉTRICAS, ENGENHARIA ELÉTRICA

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    • ABNT

      CHRISTOFF, Bruno Guilherme et al. On the strain-sensing capabilities of a novel all-solid-state sodium-based-electrolyte battery under vibration loads. Mechanical Systems and Signal Processing, v. 215, p. 1-13, 2024Tradução . . Disponível em: http://dx.doi.org/10.1016/j.ymssp.2024.111390. Acesso em: 04 nov. 2024.
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      Christoff, B. G., Marques, D., Carmo, J. P. P. do, Braga, M. H., & Tita, V. (2024). On the strain-sensing capabilities of a novel all-solid-state sodium-based-electrolyte battery under vibration loads. Mechanical Systems and Signal Processing, 215, 1-13. doi:10.1016/j.ymssp.2024.111390
    • NLM

      Christoff BG, Marques D, Carmo JPP do, Braga MH, Tita V. On the strain-sensing capabilities of a novel all-solid-state sodium-based-electrolyte battery under vibration loads [Internet]. Mechanical Systems and Signal Processing. 2024 ; 215 1-13.[citado 2024 nov. 04 ] Available from: http://dx.doi.org/10.1016/j.ymssp.2024.111390
    • Vancouver

      Christoff BG, Marques D, Carmo JPP do, Braga MH, Tita V. On the strain-sensing capabilities of a novel all-solid-state sodium-based-electrolyte battery under vibration loads [Internet]. Mechanical Systems and Signal Processing. 2024 ; 215 1-13.[citado 2024 nov. 04 ] Available from: http://dx.doi.org/10.1016/j.ymssp.2024.111390
  • Source: Theoretical and Applied Fracture Mechanics. Unidade: EESC

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

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    • 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: 04 nov. 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 nov. 04 ] 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 nov. 04 ] Available from: https://dx.doi.org/10.1016/j.tafmec.2024.104424
  • Source: Composite Structures. Unidade: EESC

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

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    • ABNT

      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: 04 nov. 2024.
    • 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 2024 nov. 04 ] 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 2024 nov. 04 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2024.118506
  • Source: Composites Science and Technology. Unidade: EESC

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

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    • 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: 04 nov. 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
    • 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 nov. 04 ] 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 nov. 04 ] Available from: https://doi.org/10.1016/j.compscitech.2022.109872
  • Source: Composite Structures. Unidade: EESC

    Subjects: MATERIAIS COMPÓSITOS, PIEZOELETRICIDADE, HOMOGENEIZAÇÃO, ENGENHARIA AERONÁUTICA

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    • ABNT

      SILVA, Matheus Rodrigues e TITA, Volnei e MEDEIROS, Ricardo de. Influence of the geometric parameters on the effective properties of piezoelectric composite sensors using real measurements and a new RVE. Composite Structures, v. 303, p. 1-12, 2023Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2022.116292. Acesso em: 04 nov. 2024.
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      Silva, M. R., Tita, V., & Medeiros, R. de. (2023). Influence of the geometric parameters on the effective properties of piezoelectric composite sensors using real measurements and a new RVE. Composite Structures, 303, 1-12. doi:10.1016/j.compstruct.2022.116292
    • NLM

      Silva MR, Tita V, Medeiros R de. Influence of the geometric parameters on the effective properties of piezoelectric composite sensors using real measurements and a new RVE [Internet]. Composite Structures. 2023 ; 303 1-12.[citado 2024 nov. 04 ] Available from: https://doi.org/10.1016/j.compstruct.2022.116292
    • Vancouver

      Silva MR, Tita V, Medeiros R de. Influence of the geometric parameters on the effective properties of piezoelectric composite sensors using real measurements and a new RVE [Internet]. Composite Structures. 2023 ; 303 1-12.[citado 2024 nov. 04 ] Available from: https://doi.org/10.1016/j.compstruct.2022.116292
  • Source: Mechanics of Advanced Materials and Structures. Unidade: EESC

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

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      POSSENTI, Kleison Antonio et al. Detection of changes in dynamic characteristics of composite structures using Kriging metamodeling procedure: Experimental and computational analysis. Mechanics of Advanced Materials and Structures, p. 1-18, 2023Tradução . . Disponível em: https://doi.org/10.1080/15376494.2023.2245816. Acesso em: 04 nov. 2024.
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      Possenti, K. A., Menezes, V. G. S. de, Vandepitte, D., Tita, V., & Medeiros, R. de. (2023). Detection of changes in dynamic characteristics of composite structures using Kriging metamodeling procedure: Experimental and computational analysis. Mechanics of Advanced Materials and Structures, 1-18. doi:10.1080/15376494.2023.2245816
    • NLM

      Possenti KA, Menezes VGS de, Vandepitte D, Tita V, Medeiros R de. Detection of changes in dynamic characteristics of composite structures using Kriging metamodeling procedure: Experimental and computational analysis [Internet]. Mechanics of Advanced Materials and Structures. 2023 ; 1-18.[citado 2024 nov. 04 ] Available from: https://doi.org/10.1080/15376494.2023.2245816
    • Vancouver

      Possenti KA, Menezes VGS de, Vandepitte D, Tita V, Medeiros R de. Detection of changes in dynamic characteristics of composite structures using Kriging metamodeling procedure: Experimental and computational analysis [Internet]. Mechanics of Advanced Materials and Structures. 2023 ; 1-18.[citado 2024 nov. 04 ] Available from: https://doi.org/10.1080/15376494.2023.2245816
  • Source: Composite Structures. Unidade: EESC

    Subjects: FADIGA DOS MATERIAIS, JUNTAS ESTRUTURAIS, ENGENHARIA AERONÁUTICA

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      MARQUES, Denys e MADUREIRA, Fernando e TITA, Volnei. Data reduction methods in the fatigue analysis of the Double Cantilever Beam, Part II: evaluation and case studies. Composite Structures, v. 324, p. 1-11, 2023Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2023.117528. Acesso em: 04 nov. 2024.
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      Marques, D., Madureira, F., & Tita, V. (2023). Data reduction methods in the fatigue analysis of the Double Cantilever Beam, Part II: evaluation and case studies. Composite Structures, 324, 1-11. doi:10.1016/j.compstruct.2023.117528
    • NLM

      Marques D, Madureira F, Tita V. Data reduction methods in the fatigue analysis of the Double Cantilever Beam, Part II: evaluation and case studies [Internet]. Composite Structures. 2023 ; 324 1-11.[citado 2024 nov. 04 ] Available from: https://doi.org/10.1016/j.compstruct.2023.117528
    • Vancouver

      Marques D, Madureira F, Tita V. Data reduction methods in the fatigue analysis of the Double Cantilever Beam, Part II: evaluation and case studies [Internet]. Composite Structures. 2023 ; 324 1-11.[citado 2024 nov. 04 ] Available from: https://doi.org/10.1016/j.compstruct.2023.117528
  • Source: Composites Part C: Open Access. Unidade: EESC

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

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      CHRISTOFF, Bruno Guilherme et al. Multiscale embedded models to determine effective mechanical properties of composite materials: asymptotic Homogenization Method combined to Finite Element Method. Composites Part C: Open Access, p. 1-14, 2022Tradução . . Disponível em: https://doi.org/10.1016/j.jcomc.2022.100303. Acesso em: 04 nov. 2024.
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      Christoff, B. G., Brito Santana, H., Talreja, R., & Tita, V. (2022). Multiscale embedded models to determine effective mechanical properties of composite materials: asymptotic Homogenization Method combined to Finite Element Method. Composites Part C: Open Access, 1-14. doi:10.1016/j.jcomc.2022.100303
    • NLM

      Christoff BG, Brito Santana H, Talreja R, Tita V. Multiscale embedded models to determine effective mechanical properties of composite materials: asymptotic Homogenization Method combined to Finite Element Method [Internet]. Composites Part C: Open Access. 2022 ; 1-14.[citado 2024 nov. 04 ] Available from: https://doi.org/10.1016/j.jcomc.2022.100303
    • Vancouver

      Christoff BG, Brito Santana H, Talreja R, Tita V. Multiscale embedded models to determine effective mechanical properties of composite materials: asymptotic Homogenization Method combined to Finite Element Method [Internet]. Composites Part C: Open Access. 2022 ; 1-14.[citado 2024 nov. 04 ] Available from: https://doi.org/10.1016/j.jcomc.2022.100303
  • Source: Fatigue & Fracture of Engineering Materials and Structures. Unidade: EESC

    Subjects: FADIGA DAS ESTRUTURAS, ESTRUTURAS, ENGENHARIA AERONÁUTICA

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      MARQUES, Denys Eduardo Teixeira e VANDEPITTE, Dirk e TITA, Volnei. Sensitivity and uncertainty analysis for structural healthmonitoring with crack propagation under random loads: anumerical framework in the frequency domain. Fatigue & Fracture of Engineering Materials and Structures, p. 1-16, 2022Tradução . . Disponível em: https://doi.org/10.1111/ffe.13853. Acesso em: 04 nov. 2024.
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      Marques, D. E. T., Vandepitte, D., & Tita, V. (2022). Sensitivity and uncertainty analysis for structural healthmonitoring with crack propagation under random loads: anumerical framework in the frequency domain. Fatigue & Fracture of Engineering Materials and Structures, 1-16. doi:10.1111/ffe.13853
    • NLM

      Marques DET, Vandepitte D, Tita V. Sensitivity and uncertainty analysis for structural healthmonitoring with crack propagation under random loads: anumerical framework in the frequency domain [Internet]. Fatigue & Fracture of Engineering Materials and Structures. 2022 ; 1-16.[citado 2024 nov. 04 ] Available from: https://doi.org/10.1111/ffe.13853
    • Vancouver

      Marques DET, Vandepitte D, Tita V. Sensitivity and uncertainty analysis for structural healthmonitoring with crack propagation under random loads: anumerical framework in the frequency domain [Internet]. Fatigue & Fracture of Engineering Materials and Structures. 2022 ; 1-16.[citado 2024 nov. 04 ] Available from: https://doi.org/10.1111/ffe.13853
  • Source: The Journal of Adhesion. Unidade: EESC

    Subjects: JUNTAS ESTRUTURAIS, VIBRAÇÕES, ENGENHARIA AERONÁUTICA

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      MADUREIRA, Fernando e SILVA, Lucas Filipe Martins da e TITA, Volnei. Compliance methods for bonded joints: part I - investigation of the standardized methods to obtain the strain energy release rate for mode I. 2022, Anais.. New York, NY, USA: Taylor & Francis, 2022. p. 1-22. Disponível em: https://doi.org/10.1080/00218464.2022.2144731. Acesso em: 04 nov. 2024.
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      Madureira, F., Silva, L. F. M. da, & Tita, V. (2022). Compliance methods for bonded joints: part I - investigation of the standardized methods to obtain the strain energy release rate for mode I. In The Journal of Adhesion (p. 1-22). New York, NY, USA: Taylor & Francis. doi:10.1080/00218464.2022.2144731
    • NLM

      Madureira F, Silva LFM da, Tita V. Compliance methods for bonded joints: part I - investigation of the standardized methods to obtain the strain energy release rate for mode I [Internet]. The Journal of Adhesion. 2022 ; 1-22.[citado 2024 nov. 04 ] Available from: https://doi.org/10.1080/00218464.2022.2144731
    • Vancouver

      Madureira F, Silva LFM da, Tita V. Compliance methods for bonded joints: part I - investigation of the standardized methods to obtain the strain energy release rate for mode I [Internet]. The Journal of Adhesion. 2022 ; 1-22.[citado 2024 nov. 04 ] Available from: https://doi.org/10.1080/00218464.2022.2144731
  • Source: Composite Structures. Unidade: EESC

    Subjects: PIEZOELETRICIDADE, HOMOGENEIZAÇÃO, ENGENHARIA AERONÁUTICA

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      GUINOVART SANJUAN, David et al. Prediction of effective properties for multilayered laminated composite with delamination: a multiscale methodology proposal. Composite Structures, v. 297, p. 1-12, 2022Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2022.115910. Acesso em: 04 nov. 2024.
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      Guinovart Sanjuan, D., Rodríguez Ramos, R., Vajravelu, K., Mohapatra, R., Guinovart Díaz, R., Brito Santana, H., et al. (2022). Prediction of effective properties for multilayered laminated composite with delamination: a multiscale methodology proposal. Composite Structures, 297, 1-12. doi:10.1016/j.compstruct.2022.115910
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      Guinovart Sanjuan D, Rodríguez Ramos R, Vajravelu K, Mohapatra R, Guinovart Díaz R, Brito Santana H, Tita V, Sabina FJ. Prediction of effective properties for multilayered laminated composite with delamination: a multiscale methodology proposal [Internet]. Composite Structures. 2022 ; 297 1-12.[citado 2024 nov. 04 ] Available from: https://doi.org/10.1016/j.compstruct.2022.115910
    • Vancouver

      Guinovart Sanjuan D, Rodríguez Ramos R, Vajravelu K, Mohapatra R, Guinovart Díaz R, Brito Santana H, Tita V, Sabina FJ. Prediction of effective properties for multilayered laminated composite with delamination: a multiscale methodology proposal [Internet]. Composite Structures. 2022 ; 297 1-12.[citado 2024 nov. 04 ] Available from: https://doi.org/10.1016/j.compstruct.2022.115910
  • 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: 04 nov. 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 nov. 04 ] 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 nov. 04 ] 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: 04 nov. 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 nov. 04 ] 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 nov. 04 ] Available from: https://doi.org/10.1016/j.compositesb.2021.109224
  • Source: Composite Structures. Unidade: EESC

    Subjects: MATERIAIS COMPÓSITOS DE FIBRAS, DANO, ENGENHARIA AERONÁUTICA

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      GONILHA, Jose A. et al. Novel progressive failure model for quasi-orthotropic pultruded FRP structures: application to compact tension and web-crippling case studies (Part II). Composite Structures, v. 255, p. 1-16, 2021Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2020.112973. Acesso em: 04 nov. 2024.
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      Gonilha, J. A., Silvestre, N., Correia, J. R., Tita, V., & Fernandes, L. A. (2021). Novel progressive failure model for quasi-orthotropic pultruded FRP structures: application to compact tension and web-crippling case studies (Part II). Composite Structures, 255, 1-16. doi:10.1016/j.compstruct.2020.112973
    • NLM

      Gonilha JA, Silvestre N, Correia JR, Tita V, Fernandes LA. Novel progressive failure model for quasi-orthotropic pultruded FRP structures: application to compact tension and web-crippling case studies (Part II) [Internet]. Composite Structures. 2021 ; 255 1-16.[citado 2024 nov. 04 ] Available from: https://doi.org/10.1016/j.compstruct.2020.112973
    • Vancouver

      Gonilha JA, Silvestre N, Correia JR, Tita V, Fernandes LA. Novel progressive failure model for quasi-orthotropic pultruded FRP structures: application to compact tension and web-crippling case studies (Part II) [Internet]. Composite Structures. 2021 ; 255 1-16.[citado 2024 nov. 04 ] Available from: https://doi.org/10.1016/j.compstruct.2020.112973
  • Source: Composite Structures. Unidade: EESC

    Subjects: DANO, MÉTODO DOS ELEMENTOS FINITOS, ENGENHARIA AERONÁUTICA

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    • ABNT

      GONILHA, Jose A. et al. Novel progressive failure model for quasi-orthotropic pultruded FRP structures: formulation and calibration of parameters (Part I). Composite Structures, v. 255, p. 1-22, 2021Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2020.112974. Acesso em: 04 nov. 2024.
    • APA

      Gonilha, J. A., Silvestre, N., Correia, J. R., Tita, V., & Martins, D. (2021). Novel progressive failure model for quasi-orthotropic pultruded FRP structures: formulation and calibration of parameters (Part I). Composite Structures, 255, 1-22. doi:10.1016/j.compstruct.2020.112974
    • NLM

      Gonilha JA, Silvestre N, Correia JR, Tita V, Martins D. Novel progressive failure model for quasi-orthotropic pultruded FRP structures: formulation and calibration of parameters (Part I) [Internet]. Composite Structures. 2021 ; 255 1-22.[citado 2024 nov. 04 ] Available from: https://doi.org/10.1016/j.compstruct.2020.112974
    • Vancouver

      Gonilha JA, Silvestre N, Correia JR, Tita V, Martins D. Novel progressive failure model for quasi-orthotropic pultruded FRP structures: formulation and calibration of parameters (Part I) [Internet]. Composite Structures. 2021 ; 255 1-22.[citado 2024 nov. 04 ] Available from: https://doi.org/10.1016/j.compstruct.2020.112974
  • Source: Thin-Walled Structures. Unidade: EESC

    Subjects: MÉTODO DOS ELEMENTOS FINITOS, LAMINADOS, AERONÁUTICA

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    • 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: 04 nov. 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 nov. 04 ] 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 nov. 04 ] Available from: https://doi.org/10.1016/j.tws.2020.107107
  • Source: Journal of Composite Materials. Unidade: EESC

    Subjects: MATERIAIS COMPÓSITOS, DANO, ENGENHARIA AERONÁUTICA

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      TONATTO, Maikson Luiz Passaia e TITA, Volnei e AMICO, Sandro Campos. Composite spirals and rings under flexural loading: experimental and numerical analysis. Journal of Composite Materials, v. 54, n. 20, p. 2697-2705, 2020Tradução . . Disponível em: https://doi.org/10.1177/0021998320902504. Acesso em: 04 nov. 2024.
    • APA

      Tonatto, M. L. P., Tita, V., & Amico, S. C. (2020). Composite spirals and rings under flexural loading: experimental and numerical analysis. Journal of Composite Materials, 54( 20), 2697-2705. doi:10.1177/0021998320902504
    • NLM

      Tonatto MLP, Tita V, Amico SC. Composite spirals and rings under flexural loading: experimental and numerical analysis [Internet]. Journal of Composite Materials. 2020 ; 54( 20): 2697-2705.[citado 2024 nov. 04 ] Available from: https://doi.org/10.1177/0021998320902504
    • Vancouver

      Tonatto MLP, Tita V, Amico SC. Composite spirals and rings under flexural loading: experimental and numerical analysis [Internet]. Journal of Composite Materials. 2020 ; 54( 20): 2697-2705.[citado 2024 nov. 04 ] Available from: https://doi.org/10.1177/0021998320902504
  • Source: Finite Elements in Analysis and Design. Unidade: EESC

    Subjects: MÉTODO DOS ELEMENTOS FINITOS, HOMOGENEIZAÇÃO, ENGENHARIA AERONÁUTICA

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      CHRISTOFF, Bruno Guilherme et al. Development of an ABAQUS™ plug-in to evaluate the fourth-order elasticity tensor of a periodic material via homogenization by the asymptotic expansion method. Finite Elements in Analysis and Design, v. 181, p. 1-13, 2020Tradução . . Disponível em: https://doi.org/10.1016/j.finel.2020.103482. Acesso em: 04 nov. 2024.
    • APA

      Christoff, B. G., Brito Santana, H., Talreja, R., & Tita, V. (2020). Development of an ABAQUS™ plug-in to evaluate the fourth-order elasticity tensor of a periodic material via homogenization by the asymptotic expansion method. Finite Elements in Analysis and Design, 181, 1-13. doi:10.1016/j.finel.2020.103482
    • NLM

      Christoff BG, Brito Santana H, Talreja R, Tita V. Development of an ABAQUS™ plug-in to evaluate the fourth-order elasticity tensor of a periodic material via homogenization by the asymptotic expansion method [Internet]. Finite Elements in Analysis and Design. 2020 ; 181 1-13.[citado 2024 nov. 04 ] Available from: https://doi.org/10.1016/j.finel.2020.103482
    • Vancouver

      Christoff BG, Brito Santana H, Talreja R, Tita V. Development of an ABAQUS™ plug-in to evaluate the fourth-order elasticity tensor of a periodic material via homogenization by the asymptotic expansion method [Internet]. Finite Elements in Analysis and Design. 2020 ; 181 1-13.[citado 2024 nov. 04 ] Available from: https://doi.org/10.1016/j.finel.2020.103482

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