Filtros : "Tita, Volnei" "Vandepitte, Dirk" "EESC" Removidos: "Indexado no Scopus" "Porto Rico" Limpar

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  • Source: Fatigue & Fracture of Engineering Materials and Structures. Unidade: EESC

    Subjects: FADIGA DAS ESTRUTURAS, ESTRUTURAS, ENGENHARIA AERONÁUTICA

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    • ABNT

      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: 03 out. 2024.
    • APA

      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 out. 03 ] 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 out. 03 ] Available from: https://doi.org/10.1111/ffe.13853
  • Source: Mechanical Systems and Signal Processing. Unidade: EESC

    Subjects: 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: 03 out. 2024.
    • APA

      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 out. 03 ] 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 out. 03 ] Available from: https://doi.org/10.1016/j.ymssp.2018.05.022
  • Source: Structural Health Monitoring. Unidade: EESC

    Subjects: MATERIAIS COMPÓSITOS DE FIBRAS, INTEGRIDADE ESTRUTURAL, VIBRAÇÕES DE AERONAVES, ENGENHARIA AERONÁUTICA

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      MEDEIROS, Ricardo de e VANDEPITTE, Dirk e TITA, Volnei. Structural health monitoring for impact damaged composite: a new methodology based on a combination of techniques. Structural Health Monitoring, v. 17, n. Ja 2018, p. 185-200, 2018Tradução . . Disponível em: https://doi.org/10.1177/1475921716688442. Acesso em: 03 out. 2024.
    • APA

      Medeiros, R. de, Vandepitte, D., & Tita, V. (2018). Structural health monitoring for impact damaged composite: a new methodology based on a combination of techniques. Structural Health Monitoring, 17( Ja 2018), 185-200. doi:10.1177/1475921716688442
    • NLM

      Medeiros R de, Vandepitte D, Tita V. Structural health monitoring for impact damaged composite: a new methodology based on a combination of techniques [Internet]. Structural Health Monitoring. 2018 ; 17( Ja 2018): 185-200.[citado 2024 out. 03 ] Available from: https://doi.org/10.1177/1475921716688442
    • Vancouver

      Medeiros R de, Vandepitte D, Tita V. Structural health monitoring for impact damaged composite: a new methodology based on a combination of techniques [Internet]. Structural Health Monitoring. 2018 ; 17( Ja 2018): 185-200.[citado 2024 out. 03 ] Available from: https://doi.org/10.1177/1475921716688442
  • Source: Anais. Conference titles: Meeting on Aeronautical Composite Materials and Structures - MACMS 2015. Unidade: EESC

    Subjects: VIBRAÇÕES DE AERONAVES, LAMINADOS, MATERIAIS COMPÓSITOS, ENGENHARIA AERONÁUTICA

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    • ABNT

      MEDEIROS, Ricardo de et al. A new structural health monitoring system for composite materials based on the combination of different methods. 2017, Anais.. São Carlos, SP: EESC-USP, 2017. Disponível em: http://soac.eesc.usp.br/index.php/macms/macms/paper/view/303/245. Acesso em: 03 out. 2024.
    • APA

      Medeiros, R. de, Tita, S. P. da S., Vandepitte, D., & Tita, V. (2017). A new structural health monitoring system for composite materials based on the combination of different methods. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/macms/macms/paper/view/303/245
    • NLM

      Medeiros R de, Tita SP da S, Vandepitte D, Tita V. A new structural health monitoring system for composite materials based on the combination of different methods [Internet]. Anais. 2017 ;[citado 2024 out. 03 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms/paper/view/303/245
    • Vancouver

      Medeiros R de, Tita SP da S, Vandepitte D, Tita V. A new structural health monitoring system for composite materials based on the combination of different methods [Internet]. Anais. 2017 ;[citado 2024 out. 03 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms/paper/view/303/245
  • Source: Mechanical Systems and Signal Processing. Unidade: EESC

    Subjects: MÉTODO DOS ELEMENTOS FINITOS, PIEZOELETRICIDADE, SENSOR, DANO

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      SARTORATO, Murilo et al. Computational model for supporting SHM systems design: damage identification via numerical analyses. Mechanical Systems and Signal Processing, v. 84, p. 445-461, 2017Tradução . . Disponível em: https://doi.org/10.1016/j.ymssp.2016.07.035. Acesso em: 03 out. 2024.
    • APA

      Sartorato, M., Medeiros, R. de, Vandepitte, D., & Tita, V. (2017). Computational model for supporting SHM systems design: damage identification via numerical analyses. Mechanical Systems and Signal Processing, 84, 445-461. doi:10.1016/j.ymssp.2016.07.035
    • NLM

      Sartorato M, Medeiros R de, Vandepitte D, Tita V. Computational model for supporting SHM systems design: damage identification via numerical analyses [Internet]. Mechanical Systems and Signal Processing. 2017 ; 84 445-461.[citado 2024 out. 03 ] Available from: https://doi.org/10.1016/j.ymssp.2016.07.035
    • Vancouver

      Sartorato M, Medeiros R de, Vandepitte D, Tita V. Computational model for supporting SHM systems design: damage identification via numerical analyses [Internet]. Mechanical Systems and Signal Processing. 2017 ; 84 445-461.[citado 2024 out. 03 ] Available from: https://doi.org/10.1016/j.ymssp.2016.07.035
  • Source: Anais. Conference titles: Meeting on Aeronautical Composite Materials and Structures - MACMS 2015. Unidade: EESC

    Subjects: LAMINADOS, MATERIAIS COMPÓSITOS, ANÁLISE EXPERIMENTAL DE ESTRUTURAS, IMPACTO DE AERONAVES, ENGENHARIA AERONÁUTICA

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      MEDEIROS, Ricardo de et al. Residual flexural strength criterion for composite plates subjected to low velocity impact. 2017, Anais.. São Carlos, SP: EESC-USP, 2017. Disponível em: http://soac.eesc.usp.br/index.php/macms/macms/paper/view/302/244. Acesso em: 03 out. 2024.
    • APA

      Medeiros, R. de, Tita, S. P. da S., Vandepitte, D., & Tita, V. (2017). Residual flexural strength criterion for composite plates subjected to low velocity impact. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/macms/macms/paper/view/302/244
    • NLM

      Medeiros R de, Tita SP da S, Vandepitte D, Tita V. Residual flexural strength criterion for composite plates subjected to low velocity impact [Internet]. Anais. 2017 ;[citado 2024 out. 03 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms/paper/view/302/244
    • Vancouver

      Medeiros R de, Tita SP da S, Vandepitte D, Tita V. Residual flexural strength criterion for composite plates subjected to low velocity impact [Internet]. Anais. 2017 ;[citado 2024 out. 03 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms/paper/view/302/244
  • Unidade: EESC

    Subjects: INTEGRIDADE ESTRUTURAL (MONITORAMENTO), MATERIAIS COMPÓSITOS (IMPACTO), MÉTODO DOS ELEMENTOS FINITOS

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    • ABNT

      MEDEIROS, Ricardo de. Development of a criterion for predicting residual strength of composite structures damaged by impact loading. 2016. Tese (Doutorado) – Universidade de São Paulo, São Carlos, 2016. Disponível em: http://www.teses.usp.br/teses/disponiveis/18/18148/tde-26072016-221608/. Acesso em: 03 out. 2024.
    • APA

      Medeiros, R. de. (2016). Development of a criterion for predicting residual strength of composite structures damaged by impact loading (Tese (Doutorado). Universidade de São Paulo, São Carlos. Recuperado de http://www.teses.usp.br/teses/disponiveis/18/18148/tde-26072016-221608/
    • NLM

      Medeiros R de. Development of a criterion for predicting residual strength of composite structures damaged by impact loading [Internet]. 2016 ;[citado 2024 out. 03 ] Available from: http://www.teses.usp.br/teses/disponiveis/18/18148/tde-26072016-221608/
    • Vancouver

      Medeiros R de. Development of a criterion for predicting residual strength of composite structures damaged by impact loading [Internet]. 2016 ;[citado 2024 out. 03 ] Available from: http://www.teses.usp.br/teses/disponiveis/18/18148/tde-26072016-221608/
  • Source: Proceedings. Conference titles: Brazilian Conference on Composite Materials. Unidade: EESC

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

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      MEDEIROS, Ricardo de et al. Computational analysis of residual flexural properties on composite plates. 2016, Anais.. Porto Alegre, RS: UFRGS, 2016. . Acesso em: 03 out. 2024.
    • APA

      Medeiros, R. de, Ribeiro, M. L., Vandepitte, D., & Tita, V. (2016). Computational analysis of residual flexural properties on composite plates. In Proceedings. Porto Alegre, RS: UFRGS.
    • NLM

      Medeiros R de, Ribeiro ML, Vandepitte D, Tita V. Computational analysis of residual flexural properties on composite plates. Proceedings. 2016 ;[citado 2024 out. 03 ]
    • Vancouver

      Medeiros R de, Ribeiro ML, Vandepitte D, Tita V. Computational analysis of residual flexural properties on composite plates. Proceedings. 2016 ;[citado 2024 out. 03 ]
  • Source: Journal of Sound and Vibration. Unidade: EESC

    Subjects: PIEZOELETRICIDADE, SENSOR, VIBRAÇÕES, DANO, MÉTODO DOS ELEMENTOS FINITOS

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      MEDEIROS, Ricardo de et al. A comparative assessment of different frequency based damage detection in unidirectional composite plates using MFC sensors. Journal of Sound and Vibration, v. No 2016, p. 171-190, 2016Tradução . . Disponível em: https://doi.org/10.1016/j.jsv.2016.06.047. Acesso em: 03 out. 2024.
    • APA

      Medeiros, R. de, Sartorato, M., Vandepitte, D., & Tita, V. (2016). A comparative assessment of different frequency based damage detection in unidirectional composite plates using MFC sensors. Journal of Sound and Vibration, No 2016, 171-190. doi:10.1016/j.jsv.2016.06.047
    • NLM

      Medeiros R de, Sartorato M, Vandepitte D, Tita V. A comparative assessment of different frequency based damage detection in unidirectional composite plates using MFC sensors [Internet]. Journal of Sound and Vibration. 2016 ; No 2016 171-190.[citado 2024 out. 03 ] Available from: https://doi.org/10.1016/j.jsv.2016.06.047
    • Vancouver

      Medeiros R de, Sartorato M, Vandepitte D, Tita V. A comparative assessment of different frequency based damage detection in unidirectional composite plates using MFC sensors [Internet]. Journal of Sound and Vibration. 2016 ; No 2016 171-190.[citado 2024 out. 03 ] Available from: https://doi.org/10.1016/j.jsv.2016.06.047
  • Source: Anais. Conference titles: International Congress of Mechanical Engineering - COBEM. Unidade: EESC

    Subjects: MATERIAIS COMPÓSITOS, LAMINADOS, AERONAVES, ENGENHARIA AERONÁUTICA

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    • ABNT

      MEDEIROS, Ricardo de et al. Residual strength criterion based on damage metric and flexural after impact (FAI) test for composite materials. 2015, Anais.. Rio de Janeiro, RJ: ABCM, 2015. . Acesso em: 03 out. 2024.
    • APA

      Medeiros, R. de, Sartorato, M., Tita, S. P. da S., Vandepitte, D., Ribeiro, M. L., & Tita, V. (2015). Residual strength criterion based on damage metric and flexural after impact (FAI) test for composite materials. In Anais. Rio de Janeiro, RJ: ABCM.
    • NLM

      Medeiros R de, Sartorato M, Tita SP da S, Vandepitte D, Ribeiro ML, Tita V. Residual strength criterion based on damage metric and flexural after impact (FAI) test for composite materials. Anais. 2015 ;[citado 2024 out. 03 ]
    • Vancouver

      Medeiros R de, Sartorato M, Tita SP da S, Vandepitte D, Ribeiro ML, Tita V. Residual strength criterion based on damage metric and flexural after impact (FAI) test for composite materials. Anais. 2015 ;[citado 2024 out. 03 ]
  • Source: Procedia Engineering. Conference titles: International Conference on Structural Integrity - ICSI. Unidade: EESC

    Subjects: ESTRUTURAS (MONITORAMENTO), VIBRAÇÕES, INTEGRIDADE ESTRUTURAL

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      MEDEIROS, Ricardo de et al. A new methodology for structural health monitoring applications. Procedia Engineering. Amsterdam: Escola de Engenharia de São Carlos, Universidade de São Paulo. Disponível em: https://doi.org/10.1016/j.proeng.2015.08.036. Acesso em: 03 out. 2024. , 2015
    • APA

      Medeiros, R. de, Lopes, H. M. R., Guedes, R. M., Vaz, M. A. P., Vandepitte, D., & Tita, V. (2015). A new methodology for structural health monitoring applications. Procedia Engineering. Amsterdam: Escola de Engenharia de São Carlos, Universidade de São Paulo. doi:10.1016/j.proeng.2015.08.036
    • NLM

      Medeiros R de, Lopes HMR, Guedes RM, Vaz MAP, Vandepitte D, Tita V. A new methodology for structural health monitoring applications [Internet]. Procedia Engineering. 2015 ; 114 54-61.[citado 2024 out. 03 ] Available from: https://doi.org/10.1016/j.proeng.2015.08.036
    • Vancouver

      Medeiros R de, Lopes HMR, Guedes RM, Vaz MAP, Vandepitte D, Tita V. A new methodology for structural health monitoring applications [Internet]. Procedia Engineering. 2015 ; 114 54-61.[citado 2024 out. 03 ] Available from: https://doi.org/10.1016/j.proeng.2015.08.036
  • Source: Composite Structures. Unidade: EESC

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

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      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: Applied Composite Materials. Unidade: EESC

    Subjects: IMPERFEIÇÕES E FALHAS DOS MATERIAIS, MATERIAIS COMPÓSITOS

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      RIBEIRO, Marcelo Leite e VANDEPITTE, Dirk e TITA, Volnei. Damage model and progressive failure analyses for filament wound composite laminates. Applied Composite Materials, v. 20, n. 5, p. 975-992, 2013Tradução . . Disponível em: https://doi.org/10.1007/s10443-013-9315-x. Acesso em: 03 out. 2024.
    • APA

      Ribeiro, M. L., Vandepitte, D., & Tita, V. (2013). Damage model and progressive failure analyses for filament wound composite laminates. Applied Composite Materials, 20( 5), 975-992. doi:10.1007/s10443-013-9315-x
    • NLM

      Ribeiro ML, Vandepitte D, Tita V. Damage model and progressive failure analyses for filament wound composite laminates [Internet]. Applied Composite Materials. 2013 ; 20( 5): 975-992.[citado 2024 out. 03 ] Available from: https://doi.org/10.1007/s10443-013-9315-x
    • Vancouver

      Ribeiro ML, Vandepitte D, Tita V. Damage model and progressive failure analyses for filament wound composite laminates [Internet]. Applied Composite Materials. 2013 ; 20( 5): 975-992.[citado 2024 out. 03 ] Available from: https://doi.org/10.1007/s10443-013-9315-x
  • Source: Proceedings of MECSOL. Conference titles: International Symposium on Solid Mechanics - MECSOL. Unidade: EESC

    Subjects: PIEZOELETRICIDADE, AERONAVES, ENGENHARIA AERONÁUTICA, ANÁLISE NUMÉRICA

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      MEDEIROS, Ricardo de et al. Numerical and experimental analyses about SHM metrics using piezoelectric materials. 2013, Anais.. Porto Alegre, RS: Escola de Engenharia de São Carlos, Universidade de São Paulo, 2013. . Acesso em: 03 out. 2024.
    • APA

      Medeiros, R. de, Sartorato, M., Ribeiro, M. L., Vandepitte, D., & Tita, V. (2013). Numerical and experimental analyses about SHM metrics using piezoelectric materials. In Proceedings of MECSOL. Porto Alegre, RS: Escola de Engenharia de São Carlos, Universidade de São Paulo.
    • NLM

      Medeiros R de, Sartorato M, Ribeiro ML, Vandepitte D, Tita V. Numerical and experimental analyses about SHM metrics using piezoelectric materials. Proceedings of MECSOL. 2013 ;[citado 2024 out. 03 ]
    • Vancouver

      Medeiros R de, Sartorato M, Ribeiro ML, Vandepitte D, Tita V. Numerical and experimental analyses about SHM metrics using piezoelectric materials. Proceedings of MECSOL. 2013 ;[citado 2024 out. 03 ]
  • Source: Proceedings of COBEM. Conference titles: International Congress of Mechanical Engineering - COBEM. Unidade: EESC

    Subjects: DANO, AERONAVES, VIBRAÇÕES

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      MEDEIROS, Ricardo de et al. Vibration-based damage identification applied for composite plate: experimental analysis. 2013, Anais.. Rio de Janeiro, RJ: ABCM, 2013. Disponível em: https://www.researchgate.net/profile/Volnei_Tita/publication/281973465_Vibration-based_damage_identification_applied_for_composite_plate_Experimental_analyses/links/5644cd7008ae54697fb81d6e/Vibration-based-damage-identification-applied-for-composite-plate-Experimental-analyses.pdf. Acesso em: 03 out. 2024.
    • APA

      Medeiros, R. de, Sartorato, M., Marques, F. D., Tita, V., & Vandepitte, D. (2013). Vibration-based damage identification applied for composite plate: experimental analysis. In Proceedings of COBEM. Rio de Janeiro, RJ: ABCM. Recuperado de https://www.researchgate.net/profile/Volnei_Tita/publication/281973465_Vibration-based_damage_identification_applied_for_composite_plate_Experimental_analyses/links/5644cd7008ae54697fb81d6e/Vibration-based-damage-identification-applied-for-composite-plate-Experimental-analyses.pdf
    • NLM

      Medeiros R de, Sartorato M, Marques FD, Tita V, Vandepitte D. Vibration-based damage identification applied for composite plate: experimental analysis [Internet]. Proceedings of COBEM. 2013 ;[citado 2024 out. 03 ] Available from: https://www.researchgate.net/profile/Volnei_Tita/publication/281973465_Vibration-based_damage_identification_applied_for_composite_plate_Experimental_analyses/links/5644cd7008ae54697fb81d6e/Vibration-based-damage-identification-applied-for-composite-plate-Experimental-analyses.pdf
    • Vancouver

      Medeiros R de, Sartorato M, Marques FD, Tita V, Vandepitte D. Vibration-based damage identification applied for composite plate: experimental analysis [Internet]. Proceedings of COBEM. 2013 ;[citado 2024 out. 03 ] Available from: https://www.researchgate.net/profile/Volnei_Tita/publication/281973465_Vibration-based_damage_identification_applied_for_composite_plate_Experimental_analyses/links/5644cd7008ae54697fb81d6e/Vibration-based-damage-identification-applied-for-composite-plate-Experimental-analyses.pdf
  • Source: Proceedings of COBEM. Conference titles: International Congress of Mechanical Engineering - COBEM. Unidade: EESC

    Subjects: INTEGRIDADE ESTRUTURAL, DANOS MECÂNICOS, VIBRAÇÕES DE AERONAVES, PIEZOELETRICIDADE, ENGENHARIA AERONÁUTICA

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      SARTORATO, Murilo et al. Vibration-based damage identification applied for composite plate: numerical analysis. 2013, Anais.. Rio de Janeiro, RJ: ABCM, 2013. . Acesso em: 03 out. 2024.
    • APA

      Sartorato, M., Medeiros, R. de, Marques, F. D., Tita, V., & Vandepitte, D. (2013). Vibration-based damage identification applied for composite plate: numerical analysis. In Proceedings of COBEM. Rio de Janeiro, RJ: ABCM.
    • NLM

      Sartorato M, Medeiros R de, Marques FD, Tita V, Vandepitte D. Vibration-based damage identification applied for composite plate: numerical analysis. Proceedings of COBEM. 2013 ;[citado 2024 out. 03 ]
    • Vancouver

      Sartorato M, Medeiros R de, Marques FD, Tita V, Vandepitte D. Vibration-based damage identification applied for composite plate: numerical analysis. Proceedings of COBEM. 2013 ;[citado 2024 out. 03 ]
  • Unidade: EESC

    Subjects: MATERIAIS COMPÓSITOS, MÉTODO DOS ELEMENTOS FINITOS, MECÂNICA DO DANO

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      RIBEIRO, Marcelo Leite. Modelos de falha e dano para estruturas aeronáuticas com curvatura e fabricadas em material compósito. 2013. Tese (Doutorado) – Universidade de São Paulo, São Carlos, 2013. Disponível em: http://www.teses.usp.br/teses/disponiveis/18/18148/tde-18112013-140301/. Acesso em: 03 out. 2024.
    • APA

      Ribeiro, M. L. (2013). Modelos de falha e dano para estruturas aeronáuticas com curvatura e fabricadas em material compósito (Tese (Doutorado). Universidade de São Paulo, São Carlos. Recuperado de http://www.teses.usp.br/teses/disponiveis/18/18148/tde-18112013-140301/
    • NLM

      Ribeiro ML. Modelos de falha e dano para estruturas aeronáuticas com curvatura e fabricadas em material compósito [Internet]. 2013 ;[citado 2024 out. 03 ] Available from: http://www.teses.usp.br/teses/disponiveis/18/18148/tde-18112013-140301/
    • Vancouver

      Ribeiro ML. Modelos de falha e dano para estruturas aeronáuticas com curvatura e fabricadas em material compósito [Internet]. 2013 ;[citado 2024 out. 03 ] Available from: http://www.teses.usp.br/teses/disponiveis/18/18148/tde-18112013-140301/
  • Source: Composite Structures. Unidade: EESC

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

    Acesso à fonteDOIHow to cite
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    • 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
  • Source: International Journal of Vehicle Structures & Systems. Unidade: EESC

    Subjects: MATERIAIS COMPÓSITOS, IMPACTO DE AERONAVES, DANO, ENGENHARIA AERONÁUTICA

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    • ABNT

      RIBEIRO, Marcelo Leite et al. Analysis of low energy impact on filament-wound composite cylinders. International Journal of Vehicle Structures & Systems, v. 4, n. 4, p. 118-122, 2012Tradução . . Disponível em: https://doi.org/10.4273/ijvss.4.4.01. Acesso em: 03 out. 2024.
    • APA

      Ribeiro, M. L., Martins, T. H. P., Sartorato, M., Ferreira, G. F. O., Tita, V., & Vandepitte, D. (2012). Analysis of low energy impact on filament-wound composite cylinders. International Journal of Vehicle Structures & Systems, 4( 4), 118-122. doi:10.4273/ijvss.4.4.01
    • NLM

      Ribeiro ML, Martins THP, Sartorato M, Ferreira GFO, Tita V, Vandepitte D. Analysis of low energy impact on filament-wound composite cylinders [Internet]. International Journal of Vehicle Structures & Systems. 2012 ; 4( 4): 118-122.[citado 2024 out. 03 ] Available from: https://doi.org/10.4273/ijvss.4.4.01
    • Vancouver

      Ribeiro ML, Martins THP, Sartorato M, Ferreira GFO, Tita V, Vandepitte D. Analysis of low energy impact on filament-wound composite cylinders [Internet]. International Journal of Vehicle Structures & Systems. 2012 ; 4( 4): 118-122.[citado 2024 out. 03 ] Available from: https://doi.org/10.4273/ijvss.4.4.01
  • Source: Proceedings. Conference titles: Brazilian Conference on Composite Materials. Unidade: EESC

    Subjects: MATERIAIS COMPÓSITOS, ESTRUTURA DE AERONAVES, ENGENHARIA AERONÁUTICA

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    • ABNT

      RIBEIRO, Marcelo Leite et al. Experimental analysis of low energy impact in filament winding cylinders. 2012, Anais.. Natal, RN: Escola de Engenharia de São Carlos, Universidade de São Paulo, 2012. Disponível em: https://repositorio.usp.br/directbitstream/5d5b97b8-e8e6-4e72-805a-9fc3ca8df9e2/trabalho%2093%20-%20Experimental%20analysis%20of%20low%20energy%20impact%20in%20filament%20winding%20cylinders%20%28BCCM%202012%29_removed.pdf. Acesso em: 03 out. 2024.
    • APA

      Ribeiro, M. L., Martins, T. H. P., Sartorato, M., Ferreira, G. F. O., Tita, V., & Vandepitte, D. (2012). Experimental analysis of low energy impact in filament winding cylinders. In Proceedings. Natal, RN: Escola de Engenharia de São Carlos, Universidade de São Paulo. Recuperado de https://repositorio.usp.br/directbitstream/5d5b97b8-e8e6-4e72-805a-9fc3ca8df9e2/trabalho%2093%20-%20Experimental%20analysis%20of%20low%20energy%20impact%20in%20filament%20winding%20cylinders%20%28BCCM%202012%29_removed.pdf
    • NLM

      Ribeiro ML, Martins THP, Sartorato M, Ferreira GFO, Tita V, Vandepitte D. Experimental analysis of low energy impact in filament winding cylinders [Internet]. Proceedings. 2012 ;[citado 2024 out. 03 ] Available from: https://repositorio.usp.br/directbitstream/5d5b97b8-e8e6-4e72-805a-9fc3ca8df9e2/trabalho%2093%20-%20Experimental%20analysis%20of%20low%20energy%20impact%20in%20filament%20winding%20cylinders%20%28BCCM%202012%29_removed.pdf
    • Vancouver

      Ribeiro ML, Martins THP, Sartorato M, Ferreira GFO, Tita V, Vandepitte D. Experimental analysis of low energy impact in filament winding cylinders [Internet]. Proceedings. 2012 ;[citado 2024 out. 03 ] Available from: https://repositorio.usp.br/directbitstream/5d5b97b8-e8e6-4e72-805a-9fc3ca8df9e2/trabalho%2093%20-%20Experimental%20analysis%20of%20low%20energy%20impact%20in%20filament%20winding%20cylinders%20%28BCCM%202012%29_removed.pdf

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