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  • Source: Composites Part B. Unidade: EESC

    Subjects: PROCESSOS DE FABRICAÇÃO, FLAMBAGEM, ENGENHARIA AERONÁUTICA

    PrivadoAcesso à fonteDOIHow to cite
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    • ABNT

      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: 11 nov. 2024.
    • APA

      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. 11 ] 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. 11 ] Available from: https://doi.org/10.1016/j.compositesb.2021.109224
  • Source: Composites Part B. Unidade: EESC

    Subjects: FLAMBAGEM, MÉTODO DOS ELEMENTOS FINITOS, ENGENHARIA AERONÁUTICA

    PrivadoAcesso à fonteDOIHow to cite
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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: 11 nov. 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 nov. 11 ] 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 nov. 11 ] Available from: https://doi.org/10.1016/j.compositesb.2018.05.004
  • Source: Composites Part B. Unidade: EESC

    Subjects: MATERIAIS COMPÓSITOS, LAMINADOS, MÉTODO DOS ELEMENTOS FINITOS

    Acesso à fonteDOIHow to cite
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    • ABNT

      CALIRI JUNIOR, Mauricio Francisco e FERREIRA, Antonio Joaquim Mendes e TITA, Volnei. Through-the-thickness stress profiles in laminated composite and sandwich structure plates via unified formulation. Composites Part B, v. 107, p. 29-42, 2016Tradução . . Disponível em: https://doi.org/10.1016/j.compositesb.2016.09.055. Acesso em: 11 nov. 2024.
    • APA

      Caliri Junior, M. F., Ferreira, A. J. M., & Tita, V. (2016). Through-the-thickness stress profiles in laminated composite and sandwich structure plates via unified formulation. Composites Part B, 107, 29-42. doi:10.1016/j.compositesb.2016.09.055
    • NLM

      Caliri Junior MF, Ferreira AJM, Tita V. Through-the-thickness stress profiles in laminated composite and sandwich structure plates via unified formulation [Internet]. Composites Part B. 2016 ; 107 29-42.[citado 2024 nov. 11 ] Available from: https://doi.org/10.1016/j.compositesb.2016.09.055
    • Vancouver

      Caliri Junior MF, Ferreira AJM, Tita V. Through-the-thickness stress profiles in laminated composite and sandwich structure plates via unified formulation [Internet]. Composites Part B. 2016 ; 107 29-42.[citado 2024 nov. 11 ] Available from: https://doi.org/10.1016/j.compositesb.2016.09.055

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