Filtros : "Tita, Volnei" "Composite Structures" "EESC" Removidos: "Indexado no Scopus" "Porto Rico" Limpar

Filtros



Refine with date range


  • Source: Composite Structures. Unidade: EESC

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

    PrivadoAcesso à fonteDOIHow to cite
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • 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: 03 out. 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 out. 03 ] 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 out. 03 ] 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

    PrivadoAcesso à fonteDOIHow to cite
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • 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: 03 out. 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 out. 03 ] 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 out. 03 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2024.118506
  • Source: Composite Structures. Unidade: EESC

    Subjects: MATERIAIS COMPÓSITOS, PIEZOELETRICIDADE, HOMOGENEIZAÇÃO, ENGENHARIA AERONÁUTICA

    PrivadoAcesso à fonteDOIHow to cite
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • 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: 03 out. 2024.
    • APA

      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 out. 03 ] 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 out. 03 ] Available from: https://doi.org/10.1016/j.compstruct.2022.116292
  • Source: Composite Structures. Unidade: EESC

    Subjects: FADIGA DOS MATERIAIS, JUNTAS ESTRUTURAIS, ENGENHARIA AERONÁUTICA

    PrivadoAcesso à fonteDOIHow to cite
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • ABNT

      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: 03 out. 2024.
    • APA

      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 out. 03 ] 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 out. 03 ] Available from: https://doi.org/10.1016/j.compstruct.2023.117528
  • Source: Composite Structures. Unidade: EESC

    Subjects: PIEZOELETRICIDADE, HOMOGENEIZAÇÃO, ENGENHARIA AERONÁUTICA

    PrivadoAcesso à fonteDOIHow to cite
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • ABNT

      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: 03 out. 2024.
    • APA

      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
    • NLM

      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 out. 03 ] 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 out. 03 ] Available from: https://doi.org/10.1016/j.compstruct.2022.115910
  • Source: Composite Structures. Unidade: EESC

    Subjects: MATERIAIS COMPÓSITOS DE FIBRAS, DANO, ENGENHARIA AERONÁUTICA

    PrivadoAcesso à fonteDOIHow to cite
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • ABNT

      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: 03 out. 2024.
    • APA

      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 out. 03 ] 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 out. 03 ] Available from: https://doi.org/10.1016/j.compstruct.2020.112973
  • Source: Composite Structures. Unidade: EESC

    Subjects: DANO, MÉTODO DOS ELEMENTOS FINITOS, ENGENHARIA AERONÁUTICA

    PrivadoAcesso à fonteDOIHow to cite
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • 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: 03 out. 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 out. 03 ] 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 out. 03 ] Available from: https://doi.org/10.1016/j.compstruct.2020.112974
  • Source: Composite Structures. Unidade: EESC

    Subjects: MATERIAIS COMPÓSITOS, MÉTODO DOS ELEMENTOS FINITOS

    PrivadoAcesso à fonteDOIHow to cite
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • ABNT

      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: 03 out. 2024.
    • APA

      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
    • NLM

      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 out. 03 ] 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 out. 03 ] Available from: https://doi.org/10.1016/j.compstruct.2019.110928
  • Source: Composite Structures. Unidade: EESC

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

    PrivadoAcesso à fonteDOIHow to cite
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • ABNT

      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: 03 out. 2024.
    • APA

      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 out. 03 ] 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 out. 03 ] Available from: https://doi.org/10.1016/j.compstruct.2018.05.085
  • Source: Composite Structures. Unidade: EESC

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

    Acesso à fonteDOIHow to cite
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • ABNT

      ALMEIDA JÚNIOR, José Humberto Santos et al. Stacking sequence optimization in composite tubes under internal pressure based on genetic algorithm accounting for progressive damage. Composite Structures, v. 178, p. 20-26, 2017Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2017.07.054. Acesso em: 03 out. 2024.
    • APA

      Almeida Júnior, J. H. S., Ribeiro, M. L., Tita, V., & Amico, S. C. (2017). Stacking sequence optimization in composite tubes under internal pressure based on genetic algorithm accounting for progressive damage. Composite Structures, 178, 20-26. doi:10.1016/j.compstruct.2017.07.054
    • NLM

      Almeida Júnior JHS, Ribeiro ML, Tita V, Amico SC. Stacking sequence optimization in composite tubes under internal pressure based on genetic algorithm accounting for progressive damage [Internet]. Composite Structures. 2017 ; 178 20-26.[citado 2024 out. 03 ] Available from: https://doi.org/10.1016/j.compstruct.2017.07.054
    • Vancouver

      Almeida Júnior JHS, Ribeiro ML, Tita V, Amico SC. Stacking sequence optimization in composite tubes under internal pressure based on genetic algorithm accounting for progressive damage [Internet]. Composite Structures. 2017 ; 178 20-26.[citado 2024 out. 03 ] Available from: https://doi.org/10.1016/j.compstruct.2017.07.054
  • Source: Composite Structures. Unidade: EESC

    Subjects: ANÁLISE NUMÉRICA, FALHA, MÉTODO DOS ELEMENTOS FINITOS

    Acesso à fonteDOIHow to cite
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • ABNT

      ALMEIDA JÚNIOR, José Humberto Santos et al. Damage modeling for carbon fiber/epoxy filament wound composite tubes under radial compression. Composite Structures, v. 160, n. Ja 2017, p. 204-210, 2017Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2016.10.036. Acesso em: 03 out. 2024.
    • APA

      Almeida Júnior, J. H. S., Ribeiro, M. L., Tita, V., & Amico, S. C. (2017). Damage modeling for carbon fiber/epoxy filament wound composite tubes under radial compression. Composite Structures, 160( Ja 2017), 204-210. doi:10.1016/j.compstruct.2016.10.036
    • NLM

      Almeida Júnior JHS, Ribeiro ML, Tita V, Amico SC. Damage modeling for carbon fiber/epoxy filament wound composite tubes under radial compression [Internet]. Composite Structures. 2017 ; 160( Ja 2017): 204-210.[citado 2024 out. 03 ] Available from: https://doi.org/10.1016/j.compstruct.2016.10.036
    • Vancouver

      Almeida Júnior JHS, Ribeiro ML, Tita V, Amico SC. Damage modeling for carbon fiber/epoxy filament wound composite tubes under radial compression [Internet]. Composite Structures. 2017 ; 160( Ja 2017): 204-210.[citado 2024 out. 03 ] Available from: https://doi.org/10.1016/j.compstruct.2016.10.036
  • Source: Composite Structures. Unidade: EESC

    Subjects: MATERIAIS COMPÓSITOS, LAMINADOS, MÉTODO DOS ELEMENTOS FINITOS

    Acesso à fonteDOIHow to cite
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • ABNT

      CALIRI JUNIOR, Mauricio Francisco e FERREIRA, António Joaquim Mendes e TITA, Volnei. A review on plate and shell theories for laminated and sandwich structures highlighting the finite element method. Composite Structures, v. No 2016, p. 63-77, 2016Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2016.02.036. Acesso em: 03 out. 2024.
    • APA

      Caliri Junior, M. F., Ferreira, A. J. M., & Tita, V. (2016). A review on plate and shell theories for laminated and sandwich structures highlighting the finite element method. Composite Structures, No 2016, 63-77. doi:10.1016/j.compstruct.2016.02.036
    • NLM

      Caliri Junior MF, Ferreira AJM, Tita V. A review on plate and shell theories for laminated and sandwich structures highlighting the finite element method [Internet]. Composite Structures. 2016 ; No 2016 63-77.[citado 2024 out. 03 ] Available from: https://doi.org/10.1016/j.compstruct.2016.02.036
    • Vancouver

      Caliri Junior MF, Ferreira AJM, Tita V. A review on plate and shell theories for laminated and sandwich structures highlighting the finite element method [Internet]. Composite Structures. 2016 ; No 2016 63-77.[citado 2024 out. 03 ] Available from: https://doi.org/10.1016/j.compstruct.2016.02.036
  • Source: Composite Structures. Unidade: EESC

    Subjects: PIEZOELETRICIDADE, MATERIAIS COMPÓSITOS, MÉTODO DOS ELEMENTOS FINITOS

    Acesso à fonteDOIHow to cite
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • ABNT

      SANTANA, Humberto Brito et al. Different interface models for calculating the effective properties in piezoelectric composite materials with imperfect fiber-matrix adhesion. Composite Structures, v. 151, p. 70-80, 2016Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2016.02.003. Acesso em: 03 out. 2024.
    • APA

      Santana, H. B., Medeiros, R. de, Rodríguez Ramos, R., & Tita, V. (2016). Different interface models for calculating the effective properties in piezoelectric composite materials with imperfect fiber-matrix adhesion. Composite Structures, 151, 70-80. doi:10.1016/j.compstruct.2016.02.003
    • NLM

      Santana HB, Medeiros R de, Rodríguez Ramos R, Tita V. Different interface models for calculating the effective properties in piezoelectric composite materials with imperfect fiber-matrix adhesion [Internet]. Composite Structures. 2016 ; 151 70-80.[citado 2024 out. 03 ] Available from: https://doi.org/10.1016/j.compstruct.2016.02.003
    • Vancouver

      Santana HB, Medeiros R de, Rodríguez Ramos R, Tita V. Different interface models for calculating the effective properties in piezoelectric composite materials with imperfect fiber-matrix adhesion [Internet]. Composite Structures. 2016 ; 151 70-80.[citado 2024 out. 03 ] Available from: https://doi.org/10.1016/j.compstruct.2016.02.003
  • Source: Composite Structures. Unidade: EESC

    Subjects: MÉTODO DOS ELEMENTOS FINITOS, ATUADORES PIEZELÉTRICOS, MATERIAIS COMPÓSITOS

    Acesso à fonteDOIHow to cite
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • ABNT

      SARTORATO, Murilo e MEDEIROS, Ricardo de e TITA, Volnei. A finite element formulation for smart piezoelectric composite shells: mathematical formulation, computational analysis and experimental evaluation. Composite Structures, v. 127, p. 185-198, 2015Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2015.03.009. Acesso em: 03 out. 2024.
    • APA

      Sartorato, M., Medeiros, R. de, & Tita, V. (2015). A finite element formulation for smart piezoelectric composite shells: mathematical formulation, computational analysis and experimental evaluation. Composite Structures, 127, 185-198. doi:10.1016/j.compstruct.2015.03.009
    • NLM

      Sartorato M, Medeiros R de, Tita V. A finite element formulation for smart piezoelectric composite shells: mathematical formulation, computational analysis and experimental evaluation [Internet]. Composite Structures. 2015 ; 127 185-198.[citado 2024 out. 03 ] Available from: https://doi.org/10.1016/j.compstruct.2015.03.009
    • Vancouver

      Sartorato M, Medeiros R de, Tita V. A finite element formulation for smart piezoelectric composite shells: mathematical formulation, computational analysis and experimental evaluation [Internet]. Composite Structures. 2015 ; 127 185-198.[citado 2024 out. 03 ] Available from: https://doi.org/10.1016/j.compstruct.2015.03.009
  • Source: Composite Structures. Unidade: EESC

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

    Acesso à fonteDOIHow to cite
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • ABNT

      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: 03 out. 2024.
    • APA

      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 out. 03 ] 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 out. 03 ] Available from: https://doi.org/10.1016/j.compstruct.2015.07.088
  • Source: Composite Structures. Unidade: EESC

    Subjects: MATERIAIS COMPÓSITOS, HOMOGENEIZAÇÃO, MÉTODO DOS ELEMENTOS FINITOS

    Acesso à fonteDOIHow to cite
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • ABNT

      RODRÍGUEZ-RAMOS, Reinaldo et al. Different approaches for calculating the effective elastic properties in composite materials under imperfect contact adherence. Composite Structures, v. 99, p. 264-275, 2013Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2012.11.040. Acesso em: 03 out. 2024.
    • APA

      Rodríguez-Ramos, R., Medeiros, R. de, Guinovart-Díaz, R., Bravo-Castillero, J., Otero, J. A., & Tita, V. (2013). Different approaches for calculating the effective elastic properties in composite materials under imperfect contact adherence. Composite Structures, 99, 264-275. doi:10.1016/j.compstruct.2012.11.040
    • NLM

      Rodríguez-Ramos R, Medeiros R de, Guinovart-Díaz R, Bravo-Castillero J, Otero JA, Tita V. Different approaches for calculating the effective elastic properties in composite materials under imperfect contact adherence [Internet]. Composite Structures. 2013 ; 99 264-275.[citado 2024 out. 03 ] Available from: https://doi.org/10.1016/j.compstruct.2012.11.040
    • Vancouver

      Rodríguez-Ramos R, Medeiros R de, Guinovart-Díaz R, Bravo-Castillero J, Otero JA, Tita V. Different approaches for calculating the effective elastic properties in composite materials under imperfect contact adherence [Internet]. Composite Structures. 2013 ; 99 264-275.[citado 2024 out. 03 ] Available from: https://doi.org/10.1016/j.compstruct.2012.11.040
  • Source: Composite Structures. Unidade: EESC

    Subjects: TERMOPLÁSTICOS, BIODEGRADAÇÃO, MÉTODO DOS ELEMENTOS FINITOS

    Acesso à fonteDOIHow to cite
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • ABNT

      VIEIRA, André Ferreira Costa e GUEDES, Rui Miranda e TITA, Volnei. Constitutive models for biodegradable thermoplastic ropes for ligament repair. Composite Structures, v. No 2012, n. 11, p. 3149-3159, 2012Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2012.05.010. Acesso em: 03 out. 2024.
    • APA

      Vieira, A. F. C., Guedes, R. M., & Tita, V. (2012). Constitutive models for biodegradable thermoplastic ropes for ligament repair. Composite Structures, No 2012( 11), 3149-3159. doi:10.1016/j.compstruct.2012.05.010
    • NLM

      Vieira AFC, Guedes RM, Tita V. Constitutive models for biodegradable thermoplastic ropes for ligament repair [Internet]. Composite Structures. 2012 ; No 2012( 11): 3149-3159.[citado 2024 out. 03 ] Available from: https://doi.org/10.1016/j.compstruct.2012.05.010
    • Vancouver

      Vieira AFC, Guedes RM, Tita V. Constitutive models for biodegradable thermoplastic ropes for ligament repair [Internet]. Composite Structures. 2012 ; No 2012( 11): 3149-3159.[citado 2024 out. 03 ] Available from: https://doi.org/10.1016/j.compstruct.2012.05.010
  • Source: Composite Structures. Unidade: EESC

    Subjects: MATERIAIS COMPÓSITOS, MATERIAIS (MODELOS), MÉTODO DOS ELEMENTOS FINITOS

    Acesso à fonteDOIHow to cite
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • ABNT

      RIBEIRO, Marcelo Leite e TITA, Volnei e VANDEPITTE, Dirk. A new damage model for composite laminates. Composite Structures, v. 94, n. Ja 2012, p. 635-642, 2012Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2011.08.031. Acesso em: 03 out. 2024.
    • APA

      Ribeiro, M. L., Tita, V., & Vandepitte, D. (2012). A new damage model for composite laminates. Composite Structures, 94( Ja 2012), 635-642. doi:10.1016/j.compstruct.2011.08.031
    • NLM

      Ribeiro ML, Tita V, Vandepitte D. A new damage model for composite laminates [Internet]. Composite Structures. 2012 ; 94( Ja 2012): 635-642.[citado 2024 out. 03 ] Available from: https://doi.org/10.1016/j.compstruct.2011.08.031
    • Vancouver

      Ribeiro ML, Tita V, Vandepitte D. A new damage model for composite laminates [Internet]. Composite Structures. 2012 ; 94( Ja 2012): 635-642.[citado 2024 out. 03 ] Available from: https://doi.org/10.1016/j.compstruct.2011.08.031

Digital Library of Intellectual Production of Universidade de São Paulo     2012 - 2024