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  • Fonte: Composites Science and Technology. Unidade: EESC

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

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      ALMEIDA JÚNIOR, José Humberto Santos et al. A concurrent fibre orientation and topology optimisation framework for 3D-printed fibre-reinforced composites. Composites Science and Technology, v. 232, p. 1-15, 2023Tradução . . Disponível em: https://doi.org/10.1016/j.compscitech.2022.109872. Acesso em: 04 ago. 2024.
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      Almeida Júnior, J. H. S., Christoff, B. G., Tita, V., & St-Pierre, L. (2023). A concurrent fibre orientation and topology optimisation framework for 3D-printed fibre-reinforced composites. Composites Science and Technology, 232, 1-15. doi:10.1016/j.compscitech.2022.109872
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      Almeida Júnior JHS, Christoff BG, Tita V, St-Pierre L. A concurrent fibre orientation and topology optimisation framework for 3D-printed fibre-reinforced composites [Internet]. Composites Science and Technology. 2023 ; 232 1-15.[citado 2024 ago. 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 ago. 04 ] Available from: https://doi.org/10.1016/j.compscitech.2022.109872
  • Fonte: Composite Structures. Unidade: EESC

    Assuntos: MATERIAIS COMPÓSITOS, PIEZOELETRICIDADE, HOMOGENEIZAÇÃO, ENGENHARIA AERONÁUTICA

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      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 ago. 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
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      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 ago. 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 ago. 04 ] Available from: https://doi.org/10.1016/j.compstruct.2022.116292
  • Fonte: Composite Structures. Unidade: EESC

    Assuntos: 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 ago. 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
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      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 ago. 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 ago. 04 ] Available from: https://doi.org/10.1016/j.compstruct.2023.117528
  • Fonte: Composites Part C: Open Access. Unidade: EESC

    Assuntos: 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 ago. 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
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      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 ago. 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 ago. 04 ] Available from: https://doi.org/10.1016/j.jcomc.2022.100303
  • Fonte: Composite Structures. Unidade: EESC

    Assuntos: 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 ago. 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 ago. 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 ago. 04 ] Available from: https://doi.org/10.1016/j.compstruct.2022.115910
  • Fonte: Thin-Walled Structures. Unidade: EESC

    Assuntos: 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 ago. 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
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      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 ago. 04 ] Available from: https://doi.org/10.1016/j.tws.2021.108864
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      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 ago. 04 ] Available from: https://doi.org/10.1016/j.tws.2021.108864
  • Fonte: Composites Part B. Unidade: EESC

    Assuntos: 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 ago. 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
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      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 ago. 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 ago. 04 ] Available from: https://doi.org/10.1016/j.compositesb.2021.109224
  • Fonte: Composite Structures. Unidade: EESC

    Assuntos: 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 ago. 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
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      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 ago. 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 ago. 04 ] Available from: https://doi.org/10.1016/j.compstruct.2020.112973
  • Fonte: Composite Structures. Unidade: EESC

    Assuntos: DANO, MÉTODO DOS ELEMENTOS FINITOS, ENGENHARIA AERONÁUTICA

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      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 ago. 2024.
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      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
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      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 ago. 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 ago. 04 ] Available from: https://doi.org/10.1016/j.compstruct.2020.112974
  • Fonte: Finite Elements in Analysis and Design. Unidade: EESC

    Assuntos: 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 ago. 2024.
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      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
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      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 ago. 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 ago. 04 ] Available from: https://doi.org/10.1016/j.finel.2020.103482
  • Fonte: Composite Structures. Unidade: EESC

    Assuntos: MATERIAIS COMPÓSITOS, MÉTODO DOS ELEMENTOS FINITOS

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      ALMEIDA JÚNIOR, José Humberto Santos et al. Buckling optimization of composite cylinders for axial compression: A design methodology considering a variable-axial fiber layout. Composite Structures, v. 222, p. 1-12, 2019Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2019.110928. Acesso em: 04 ago. 2024.
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      Almeida Júnior, J. H. S., Bittrich, L., Jansen, E., Tita, V., & Spickenheuer, A. (2019). Buckling optimization of composite cylinders for axial compression: A design methodology considering a variable-axial fiber layout. Composite Structures, 222, 1-12. doi:10.1016/j.compstruct.2019.110928
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      Almeida Júnior JHS, Bittrich L, Jansen E, Tita V, Spickenheuer A. Buckling optimization of composite cylinders for axial compression: A design methodology considering a variable-axial fiber layout [Internet]. Composite Structures. 2019 ; 222 1-12.[citado 2024 ago. 04 ] Available from: https://doi.org/10.1016/j.compstruct.2019.110928
    • Vancouver

      Almeida Júnior JHS, Bittrich L, Jansen E, Tita V, Spickenheuer A. Buckling optimization of composite cylinders for axial compression: A design methodology considering a variable-axial fiber layout [Internet]. Composite Structures. 2019 ; 222 1-12.[citado 2024 ago. 04 ] Available from: https://doi.org/10.1016/j.compstruct.2019.110928
  • Fonte: Mechanical Systems and Signal Processing. Unidade: EESC

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

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      SOUZA, Luiz Fernando dos Santos et al. Dynamic response of laminated composites using design of experiments: an experimental and numerical study. Mechanical Systems and Signal Processing, v. 115, p. 82-101, 2019Tradução . . Disponível em: https://doi.org/10.1016/j.ymssp.2018.05.022. Acesso em: 04 ago. 2024.
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      Souza, L. F. dos S., Vandepitte, D., Tita, V., & Medeiros, R. de. (2019). Dynamic response of laminated composites using design of experiments: an experimental and numerical study. Mechanical Systems and Signal Processing, 115, 82-101. doi:10.1016/j.ymssp.2018.05.022
    • NLM

      Souza LF dos S, Vandepitte D, Tita V, Medeiros R de. Dynamic response of laminated composites using design of experiments: an experimental and numerical study [Internet]. Mechanical Systems and Signal Processing. 2019 ; 115 82-101.[citado 2024 ago. 04 ] Available from: https://doi.org/10.1016/j.ymssp.2018.05.022
    • Vancouver

      Souza LF dos S, Vandepitte D, Tita V, Medeiros R de. Dynamic response of laminated composites using design of experiments: an experimental and numerical study [Internet]. Mechanical Systems and Signal Processing. 2019 ; 115 82-101.[citado 2024 ago. 04 ] Available from: https://doi.org/10.1016/j.ymssp.2018.05.022
  • Fonte: Applied Mathematical Modelling. Unidade: EESC

    Assuntos: HOMOGENEIZAÇÃO, MÉTODO DOS ELEMENTOS FINITOS

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      SANTANA, Humberto Brito et al. Multiscale analysis for predicting the constitutive tensor effective coefficients of layered composites with micro and macro failures. Applied Mathematical Modelling, v. 75, p. 250-266, 2019Tradução . . Disponível em: https://doi.org/10.1016/j.apm.2019.05.031. Acesso em: 04 ago. 2024.
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      Santana, H. B., Thiesen, J. L. M., Medeiros, R. de, Ferreira, A. J. M., Rodríguez Ramos, R., & Tita, V. (2019). Multiscale analysis for predicting the constitutive tensor effective coefficients of layered composites with micro and macro failures. Applied Mathematical Modelling, 75, 250-266. doi:10.1016/j.apm.2019.05.031
    • NLM

      Santana HB, Thiesen JLM, Medeiros R de, Ferreira AJM, Rodríguez Ramos R, Tita V. Multiscale analysis for predicting the constitutive tensor effective coefficients of layered composites with micro and macro failures [Internet]. Applied Mathematical Modelling. 2019 ; 75 250-266.[citado 2024 ago. 04 ] Available from: https://doi.org/10.1016/j.apm.2019.05.031
    • Vancouver

      Santana HB, Thiesen JLM, Medeiros R de, Ferreira AJM, Rodríguez Ramos R, Tita V. Multiscale analysis for predicting the constitutive tensor effective coefficients of layered composites with micro and macro failures [Internet]. Applied Mathematical Modelling. 2019 ; 75 250-266.[citado 2024 ago. 04 ] Available from: https://doi.org/10.1016/j.apm.2019.05.031
  • Fonte: Marine composites: design and performance. Unidade: EESC

    Assuntos: ESTRUTURAS OFFSHORE, ENGENHARIA AERONÁUTICA

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      TONATTO, Maikson Luiz Passaia et al. Offloading marine hoses: computational and experimental analyses. Marine composites: design and performance. Tradução . Kidlington, United Kingdom: Elsevier, 2019. . Disponível em: https://repositorio.usp.br/directbitstream/b47af7db-da8b-4cd8-accc-f61345c46192/PROD_25272_SYSNO_3102802.pdf. Acesso em: 04 ago. 2024.
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      Tonatto, M. L. P., Roese, P. B., Tita, V., Forte, M. M. de C., & Amico, S. C. (2019). Offloading marine hoses: computational and experimental analyses. In Marine composites: design and performance. Kidlington, United Kingdom: Elsevier. Recuperado de https://repositorio.usp.br/directbitstream/b47af7db-da8b-4cd8-accc-f61345c46192/PROD_25272_SYSNO_3102802.pdf
    • NLM

      Tonatto MLP, Roese PB, Tita V, Forte MM de C, Amico SC. Offloading marine hoses: computational and experimental analyses [Internet]. In: Marine composites: design and performance. Kidlington, United Kingdom: Elsevier; 2019. [citado 2024 ago. 04 ] Available from: https://repositorio.usp.br/directbitstream/b47af7db-da8b-4cd8-accc-f61345c46192/PROD_25272_SYSNO_3102802.pdf
    • Vancouver

      Tonatto MLP, Roese PB, Tita V, Forte MM de C, Amico SC. Offloading marine hoses: computational and experimental analyses [Internet]. In: Marine composites: design and performance. Kidlington, United Kingdom: Elsevier; 2019. [citado 2024 ago. 04 ] Available from: https://repositorio.usp.br/directbitstream/b47af7db-da8b-4cd8-accc-f61345c46192/PROD_25272_SYSNO_3102802.pdf
  • Fonte: Marine Structures. Unidade: EESC

    Assuntos: MÉTODO DOS ELEMENTOS FINITOS, ENGENHARIA AERONÁUTICA

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      TONATTO, Maikson Luiz Passaia et al. Multi-scale analyses of a floating marine hose with hybrid polyaramid/polyamide reinforcement cords. Marine Structures, v. 60, p. 279-292, 2018Tradução . . Disponível em: https://doi.org/10.1016/j.marstruc.2018.04.005. Acesso em: 04 ago. 2024.
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      Tonatto, M. L. P., Tita, V., Forte, M. M. C., & Amico, S. C. (2018). Multi-scale analyses of a floating marine hose with hybrid polyaramid/polyamide reinforcement cords. Marine Structures, 60, 279-292. doi:10.1016/j.marstruc.2018.04.005
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      Tonatto MLP, Tita V, Forte MMC, Amico SC. Multi-scale analyses of a floating marine hose with hybrid polyaramid/polyamide reinforcement cords [Internet]. Marine Structures. 2018 ; 60 279-292.[citado 2024 ago. 04 ] Available from: https://doi.org/10.1016/j.marstruc.2018.04.005
    • Vancouver

      Tonatto MLP, Tita V, Forte MMC, Amico SC. Multi-scale analyses of a floating marine hose with hybrid polyaramid/polyamide reinforcement cords [Internet]. Marine Structures. 2018 ; 60 279-292.[citado 2024 ago. 04 ] Available from: https://doi.org/10.1016/j.marstruc.2018.04.005
  • Fonte: Composite Structures. Unidade: EESC

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

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      RIBEIRO, Marcelo Leite et al. Experimental and numerical dynamic analysis of laminate plates via Carrera Unified Formulation. Composite Structures, v. 202, p. 1176-1185, 2018Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2018.05.085. Acesso em: 04 ago. 2024.
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      Ribeiro, M. L., Ferreira, G. F. O., Medeiros, R. de, Ferreira, A. J. M., & Tita, V. (2018). Experimental and numerical dynamic analysis of laminate plates via Carrera Unified Formulation. Composite Structures, 202, 1176-1185. doi:10.1016/j.compstruct.2018.05.085
    • NLM

      Ribeiro ML, Ferreira GFO, Medeiros R de, Ferreira AJM, Tita V. Experimental and numerical dynamic analysis of laminate plates via Carrera Unified Formulation [Internet]. Composite Structures. 2018 ; 202 1176-1185.[citado 2024 ago. 04 ] Available from: https://doi.org/10.1016/j.compstruct.2018.05.085
    • Vancouver

      Ribeiro ML, Ferreira GFO, Medeiros R de, Ferreira AJM, Tita V. Experimental and numerical dynamic analysis of laminate plates via Carrera Unified Formulation [Internet]. Composite Structures. 2018 ; 202 1176-1185.[citado 2024 ago. 04 ] Available from: https://doi.org/10.1016/j.compstruct.2018.05.085
  • Fonte: Applied Mathematical Modelling. Unidade: EESC

    Assuntos: 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

      SANTANA, Humberto Brito et al. Effective elastic properties of layered composites considering non-uniform imperfect adhesion. Applied Mathematical Modelling, v. 59, p. 183-204, 2018Tradução . . Disponível em: https://doi.org/10.1016/j.apm.2018.01.009. Acesso em: 04 ago. 2024.
    • APA

      Santana, H. B., Medeiros, R. de, Ferreira, A. J. M., Rodríguez Ramos, R., & Tita, V. (2018). Effective elastic properties of layered composites considering non-uniform imperfect adhesion. Applied Mathematical Modelling, 59, 183-204. doi:10.1016/j.apm.2018.01.009
    • NLM

      Santana HB, Medeiros R de, Ferreira AJM, Rodríguez Ramos R, Tita V. Effective elastic properties of layered composites considering non-uniform imperfect adhesion [Internet]. Applied Mathematical Modelling. 2018 ; 59 183-204.[citado 2024 ago. 04 ] Available from: https://doi.org/10.1016/j.apm.2018.01.009
    • Vancouver

      Santana HB, Medeiros R de, Ferreira AJM, Rodríguez Ramos R, Tita V. Effective elastic properties of layered composites considering non-uniform imperfect adhesion [Internet]. Applied Mathematical Modelling. 2018 ; 59 183-204.[citado 2024 ago. 04 ] Available from: https://doi.org/10.1016/j.apm.2018.01.009
  • Fonte: Composites Part B. Unidade: EESC

    Assuntos: FLAMBAGEM, MÉTODO DOS ELEMENTOS FINITOS, ENGENHARIA AERONÁUTICA

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    • 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: 04 ago. 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 ago. 04 ] 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 ago. 04 ] Available from: https://doi.org/10.1016/j.compositesb.2018.05.004

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