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  • Source: Additive Manufacturing. Unidade: EESC

    Subjects: EXTRUSÃO, MANUFATURA ADITIVA, MATERIAIS

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      JUSTINO NETTO, Joaquim Manoel et al. Design and validation of an innovative 3D printer containing a co-rotating twin screw extrusion unit. Additive Manufacturing, v. 59, p. 1-14, 2022Tradução . . Disponível em: https://doi.org/10.1016/j.addma.2022.103192. Acesso em: 15 jun. 2024.
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      Justino Netto, J. M., Sarout, A. I., Santos, A. L. G., Lucas, A. de A., Chinelatto, M. A., Alves, jorge L., et al. (2022). Design and validation of an innovative 3D printer containing a co-rotating twin screw extrusion unit. Additive Manufacturing, 59, 1-14. doi:10.1016/j.addma.2022.103192
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      Justino Netto JM, Sarout AI, Santos ALG, Lucas A de A, Chinelatto MA, Alves jorge L, Cunha AG, Covas JA, Silveira Z de. Design and validation of an innovative 3D printer containing a co-rotating twin screw extrusion unit [Internet]. Additive Manufacturing. 2022 ; 59 1-14.[citado 2024 jun. 15 ] Available from: https://doi.org/10.1016/j.addma.2022.103192
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      Justino Netto JM, Sarout AI, Santos ALG, Lucas A de A, Chinelatto MA, Alves jorge L, Cunha AG, Covas JA, Silveira Z de. Design and validation of an innovative 3D printer containing a co-rotating twin screw extrusion unit [Internet]. Additive Manufacturing. 2022 ; 59 1-14.[citado 2024 jun. 15 ] Available from: https://doi.org/10.1016/j.addma.2022.103192
  • Source: Case Studies on Transport Policy. Unidade: EESC

    Subjects: ACIDENTES DE TRÂNSITO, COMPORTAMENTO DE RISCO, TRANSPORTES

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      CAMPOS, Cintia Isabel de et al. What are the risk behaviors of Brazilian and Portuguese drivers?: an exploratory approach using self-reported data. Case Studies on Transport Policy, v. 9, n. 4, p. 1746-1756, 2021Tradução . . Disponível em: https://doi.org/10.1016/j.cstp.2021.07.021. Acesso em: 15 jun. 2024.
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      Campos, C. I. de, Pitombo, C. S., Delhomme, P., & Ferreira, S. (2021). What are the risk behaviors of Brazilian and Portuguese drivers?: an exploratory approach using self-reported data. Case Studies on Transport Policy, 9( 4), 1746-1756. doi:10.1016/j.cstp.2021.07.021
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      Campos CI de, Pitombo CS, Delhomme P, Ferreira S. What are the risk behaviors of Brazilian and Portuguese drivers?: an exploratory approach using self-reported data [Internet]. Case Studies on Transport Policy. 2021 ; 9( 4): 1746-1756.[citado 2024 jun. 15 ] Available from: https://doi.org/10.1016/j.cstp.2021.07.021
    • Vancouver

      Campos CI de, Pitombo CS, Delhomme P, Ferreira S. What are the risk behaviors of Brazilian and Portuguese drivers?: an exploratory approach using self-reported data [Internet]. Case Studies on Transport Policy. 2021 ; 9( 4): 1746-1756.[citado 2024 jun. 15 ] Available from: https://doi.org/10.1016/j.cstp.2021.07.021
  • Source: Applied Mathematical Modelling. Unidade: EESC

    Subjects: 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: 15 jun. 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 jun. 15 ] Available from: https://doi.org/10.1016/j.apm.2019.05.031
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      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 jun. 15 ] Available from: https://doi.org/10.1016/j.apm.2019.05.031
  • Source: Composite Structures. Unidade: EESC

    Subjects: 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: 15 jun. 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 jun. 15 ] Available from: https://doi.org/10.1016/j.compstruct.2018.05.085
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      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 jun. 15 ] Available from: https://doi.org/10.1016/j.compstruct.2018.05.085
  • Source: International Journal of Non-Linear Mechanics. Unidade: EESC

    Subjects: AEROELASTICIDADE DE AERONAVES, VIBRAÇÕES DE AERONAVES, ENGENHARIA MECÂNICA

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      PACHECO, Douglas Ramalho Queiroz e MARQUES, Flavio Donizeti e FERREIRA, Antonio Joaquim Mendes. Panel flutter suppression with nonlinear energy sinks: numerical modeling and analysis. International Journal of Non-Linear Mechanics, v. 106, p. 108-114, 2018Tradução . . Disponível em: https://doi.org/10.1016/j.ijnonlinmec.2018.08.009. Acesso em: 15 jun. 2024.
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      Pacheco, D. R. Q., Marques, F. D., & Ferreira, A. J. M. (2018). Panel flutter suppression with nonlinear energy sinks: numerical modeling and analysis. International Journal of Non-Linear Mechanics, 106, 108-114. doi:10.1016/j.ijnonlinmec.2018.08.009
    • NLM

      Pacheco DRQ, Marques FD, Ferreira AJM. Panel flutter suppression with nonlinear energy sinks: numerical modeling and analysis [Internet]. International Journal of Non-Linear Mechanics. 2018 ; 106 108-114.[citado 2024 jun. 15 ] Available from: https://doi.org/10.1016/j.ijnonlinmec.2018.08.009
    • Vancouver

      Pacheco DRQ, Marques FD, Ferreira AJM. Panel flutter suppression with nonlinear energy sinks: numerical modeling and analysis [Internet]. International Journal of Non-Linear Mechanics. 2018 ; 106 108-114.[citado 2024 jun. 15 ] Available from: https://doi.org/10.1016/j.ijnonlinmec.2018.08.009
  • Source: Applied Mathematical Modelling. Unidade: EESC

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

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      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: 15 jun. 2024.
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      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 jun. 15 ] 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 jun. 15 ] Available from: https://doi.org/10.1016/j.apm.2018.01.009
  • Source: Journal of Sound and Vibration. Unidade: EESC

    Subjects: AERODINÂMICA DE AERONAVES, MÉTODO DOS ELEMENTOS FINITOS, ENGENHARIA MECÂNICA

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      PACHECO, Douglas Ramalho Queiroz e MARQUES, Flavio Donizeti e FERREIRA, Antonio Joaquim Mendes. Finite element analysis of fluttering plates reinforced by flexible beams: an energy-based approach. Journal of Sound and Vibration, v. 435, p. 135-148, 2018Tradução . . Disponível em: https://doi.org/10.1016/j.jsv.2018.07.042. Acesso em: 15 jun. 2024.
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      Pacheco, D. R. Q., Marques, F. D., & Ferreira, A. J. M. (2018). Finite element analysis of fluttering plates reinforced by flexible beams: an energy-based approach. Journal of Sound and Vibration, 435, 135-148. doi:10.1016/j.jsv.2018.07.042
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      Pacheco DRQ, Marques FD, Ferreira AJM. Finite element analysis of fluttering plates reinforced by flexible beams: an energy-based approach [Internet]. Journal of Sound and Vibration. 2018 ; 435 135-148.[citado 2024 jun. 15 ] Available from: https://doi.org/10.1016/j.jsv.2018.07.042
    • Vancouver

      Pacheco DRQ, Marques FD, Ferreira AJM. Finite element analysis of fluttering plates reinforced by flexible beams: an energy-based approach [Internet]. Journal of Sound and Vibration. 2018 ; 435 135-148.[citado 2024 jun. 15 ] Available from: https://doi.org/10.1016/j.jsv.2018.07.042
  • Source: Journal of Fluids and Structures. Unidade: EESC

    Assunto: ENGENHARIA MECÂNICA

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      PACHECO, Douglas Ramalho Queiroz e FERREIRA, Antonio Joaquim Mendes e MARQUES, Flavio Donizeti. On the effects of structural coupling on the supersonic flutter and limit cycle oscillations of transversely reinforced panels. Journal of Fluids and Structures, v. 79, p. 158-170, 2018Tradução . . Disponível em: https://doi.org/10.1016/j.jfluidstructs.2018.01.013. Acesso em: 15 jun. 2024.
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      Pacheco, D. R. Q., Ferreira, A. J. M., & Marques, F. D. (2018). On the effects of structural coupling on the supersonic flutter and limit cycle oscillations of transversely reinforced panels. Journal of Fluids and Structures, 79, 158-170. doi:10.1016/j.jfluidstructs.2018.01.013
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      Pacheco DRQ, Ferreira AJM, Marques FD. On the effects of structural coupling on the supersonic flutter and limit cycle oscillations of transversely reinforced panels [Internet]. Journal of Fluids and Structures. 2018 ; 79 158-170.[citado 2024 jun. 15 ] Available from: https://doi.org/10.1016/j.jfluidstructs.2018.01.013
    • Vancouver

      Pacheco DRQ, Ferreira AJM, Marques FD. On the effects of structural coupling on the supersonic flutter and limit cycle oscillations of transversely reinforced panels [Internet]. Journal of Fluids and Structures. 2018 ; 79 158-170.[citado 2024 jun. 15 ] Available from: https://doi.org/10.1016/j.jfluidstructs.2018.01.013
  • Source: Composite Structures. Unidade: EESC

    Subjects: AEROELASTICIDADE DE AERONAVES, MÉTODO DOS ELEMENTOS FINITOS, VIBRAÇÕES DE AERONAVES, ENGENHARIA MECÂNICA

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      PACHECO, D. R. Q. et al. Nonlinear finite element post-flutter analysis of multibay composite panels in supersonic regime. Composite Structures, v. 180, p. 883-891, 2017Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2017.08.058. Acesso em: 15 jun. 2024.
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      Pacheco, D. R. Q., Marques, F. D., Natarajan, S., & Ferreira, A. J. M. (2017). Nonlinear finite element post-flutter analysis of multibay composite panels in supersonic regime. Composite Structures, 180, 883-891. doi:10.1016/j.compstruct.2017.08.058
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      Pacheco DRQ, Marques FD, Natarajan S, Ferreira AJM. Nonlinear finite element post-flutter analysis of multibay composite panels in supersonic regime [Internet]. Composite Structures. 2017 ; 180 883-891.[citado 2024 jun. 15 ] Available from: https://doi.org/10.1016/j.compstruct.2017.08.058
    • Vancouver

      Pacheco DRQ, Marques FD, Natarajan S, Ferreira AJM. Nonlinear finite element post-flutter analysis of multibay composite panels in supersonic regime [Internet]. Composite Structures. 2017 ; 180 883-891.[citado 2024 jun. 15 ] Available from: https://doi.org/10.1016/j.compstruct.2017.08.058
  • Source: Thin-Walled Structures. Unidade: EESC

    Subjects: AEROELASTICIDADE DE AERONAVES, MÉTODO DOS ELEMENTOS FINITOS, ESCOAMENTO, ENGENHARIA MECÂNICA

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      PACHECO, D. R. Q. e MARQUES, Flavio Donizeti e FERREIRA, A. J. M. Nonlinear finite element aeroelastic analysis of multibay panels in supersonic flow regime. Thin-Walled Structures, v. 120, p. 470-478, 2017Tradução . . Disponível em: https://doi.org/10.1016/j.tws.2017.08.034. Acesso em: 15 jun. 2024.
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      Pacheco, D. R. Q., Marques, F. D., & Ferreira, A. J. M. (2017). Nonlinear finite element aeroelastic analysis of multibay panels in supersonic flow regime. Thin-Walled Structures, 120, 470-478. doi:10.1016/j.tws.2017.08.034
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      Pacheco DRQ, Marques FD, Ferreira AJM. Nonlinear finite element aeroelastic analysis of multibay panels in supersonic flow regime [Internet]. Thin-Walled Structures. 2017 ; 120 470-478.[citado 2024 jun. 15 ] Available from: https://doi.org/10.1016/j.tws.2017.08.034
    • Vancouver

      Pacheco DRQ, Marques FD, Ferreira AJM. Nonlinear finite element aeroelastic analysis of multibay panels in supersonic flow regime [Internet]. Thin-Walled Structures. 2017 ; 120 470-478.[citado 2024 jun. 15 ] Available from: https://doi.org/10.1016/j.tws.2017.08.034

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