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  • Source: Composite Structures. Unidade: EESC

    Subjects: MATERIAIS COMPÓSITOS, LAMINADOS, ENGENHARIA MECÂNICA

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      LEMOS, Diego Magela e MARQUES, Flavio Donizeti e FERREIRA, Antonio Joaquim Mendes. A review on bistable composite laminates for aerospace applications. Composite Structures, v. 329, p. 1-21, 2024Tradução . . Disponível em: http://dx.doi.org/10.1016/j.compstruct.2023.117756. Acesso em: 13 jun. 2024.
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      Lemos, D. M., Marques, F. D., & Ferreira, A. J. M. (2024). A review on bistable composite laminates for aerospace applications. Composite Structures, 329, 1-21. doi:10.1016/j.compstruct.2023.117756
    • NLM

      Lemos DM, Marques FD, Ferreira AJM. A review on bistable composite laminates for aerospace applications [Internet]. Composite Structures. 2024 ; 329 1-21.[citado 2024 jun. 13 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2023.117756
    • Vancouver

      Lemos DM, Marques FD, Ferreira AJM. A review on bistable composite laminates for aerospace applications [Internet]. Composite Structures. 2024 ; 329 1-21.[citado 2024 jun. 13 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2023.117756
  • Source: Physics of Fluids. Unidade: EESC

    Subjects: TEMPO-REAL, AERONAVES, ASAS DE AERONAVES, ENGENHARIA MECÂNICA

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      CAMACHO, Emanuel A. R. et al. Real-time optimization of wing drag and lift performance using a movable leading edge. Physics of Fluids, v. 36, n. 1, p. 1-11, 2024Tradução . . Disponível em: https://dx.doi.org/10.1063/5.0185716. Acesso em: 13 jun. 2024.
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      Camacho, E. A. R., Silva, M. M. da, Silva, A. R. R., & Marques, F. D. (2024). Real-time optimization of wing drag and lift performance using a movable leading edge. Physics of Fluids, 36( 1), 1-11. doi:10.1063/5.0185716
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      Camacho EAR, Silva MM da, Silva ARR, Marques FD. Real-time optimization of wing drag and lift performance using a movable leading edge [Internet]. Physics of Fluids. 2024 ; 36( 1): 1-11.[citado 2024 jun. 13 ] Available from: https://dx.doi.org/10.1063/5.0185716
    • Vancouver

      Camacho EAR, Silva MM da, Silva ARR, Marques FD. Real-time optimization of wing drag and lift performance using a movable leading edge [Internet]. Physics of Fluids. 2024 ; 36( 1): 1-11.[citado 2024 jun. 13 ] Available from: https://dx.doi.org/10.1063/5.0185716
  • Source: Energies. Unidade: EESC

    Subjects: ENGENHARIA MECÂNICA, MICROPROCESSADORES, DISPOSITIVOS ELETRÔNICOS, BATERIAS ELÉTRICAS

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      AMORIM, Marcio L. M. et al. Low-cost/high-precision smart power supply for data loggers. Energies, v. 16, n. 1, p. 1-27, 2023Tradução . . Disponível em: https://doi.org/10.3390/en16010278. Acesso em: 13 jun. 2024.
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      Amorim, M. L. M., Ginja, ^G. ^A., Carmo, J. P. P. do, Moreira, M. de M. A. C., Siqueira, A. A. G., & Afonso, J. A. (2023). Low-cost/high-precision smart power supply for data loggers. Energies, 16( 1), 1-27. doi:10.3390/en16010278
    • NLM

      Amorim MLM, Ginja ^G^A, Carmo JPP do, Moreira M de MAC, Siqueira AAG, Afonso JA. Low-cost/high-precision smart power supply for data loggers [Internet]. Energies. 2023 ; 16( 1): 1-27.[citado 2024 jun. 13 ] Available from: https://doi.org/10.3390/en16010278
    • Vancouver

      Amorim MLM, Ginja ^G^A, Carmo JPP do, Moreira M de MAC, Siqueira AAG, Afonso JA. Low-cost/high-precision smart power supply for data loggers [Internet]. Energies. 2023 ; 16( 1): 1-27.[citado 2024 jun. 13 ] Available from: https://doi.org/10.3390/en16010278
  • Source: Engineering Proceedings. Unidade: EESC

    Subjects: AEROFÓLIOS, PROPULSÃO DE AERONAVES, ENGENHARIA MECÂNICA

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      CAMACHO, Emanuel A. R e MARQUES, Flavio Donizeti e SILVA, Andre R. R. Predicting the NACA0012-IK30 airfoil propulsive capabilities with a panel method. Engineering Proceedings, v. 56, n. 1, p. 1-8, 2023Tradução . . Disponível em: https://dx.doi.org/10.3390/ASEC2023-15886. Acesso em: 13 jun. 2024.
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      Camacho, E. A. R., Marques, F. D., & Silva, A. R. R. (2023). Predicting the NACA0012-IK30 airfoil propulsive capabilities with a panel method. Engineering Proceedings, 56( 1), 1-8. doi:10.3390/ASEC2023-15886
    • NLM

      Camacho EAR, Marques FD, Silva ARR. Predicting the NACA0012-IK30 airfoil propulsive capabilities with a panel method [Internet]. Engineering Proceedings. 2023 ; 56( 1): 1-8.[citado 2024 jun. 13 ] Available from: https://dx.doi.org/10.3390/ASEC2023-15886
    • Vancouver

      Camacho EAR, Marques FD, Silva ARR. Predicting the NACA0012-IK30 airfoil propulsive capabilities with a panel method [Internet]. Engineering Proceedings. 2023 ; 56( 1): 1-8.[citado 2024 jun. 13 ] Available from: https://dx.doi.org/10.3390/ASEC2023-15886
  • Source: Engineering Proceedings. Unidade: EESC

    Subjects: PETRÓLEO, GASES, APRENDIZADO COMPUTACIONAL, AERODINÂMICA, REDES NEURAIS, ENGENHARIA MECÂNICA

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      PEREIRA, João A. F. et al. Fast flapping aerodynamics prediction using a recurrent neural network. Engineering Proceedings, v. 56, n. 1, p. 1-7, 2023Tradução . . Disponível em: https://dx.doi.org/10.3390/ASEC2023-16272. Acesso em: 13 jun. 2024.
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      Pereira, J. A. F., Camacho, E. A. R., Marques, F. D., & Silva, A. R. R. (2023). Fast flapping aerodynamics prediction using a recurrent neural network. Engineering Proceedings, 56( 1), 1-7. doi:10.3390/ASEC2023-16272
    • NLM

      Pereira JAF, Camacho EAR, Marques FD, Silva ARR. Fast flapping aerodynamics prediction using a recurrent neural network [Internet]. Engineering Proceedings. 2023 ; 56( 1): 1-7.[citado 2024 jun. 13 ] Available from: https://dx.doi.org/10.3390/ASEC2023-16272
    • Vancouver

      Pereira JAF, Camacho EAR, Marques FD, Silva ARR. Fast flapping aerodynamics prediction using a recurrent neural network [Internet]. Engineering Proceedings. 2023 ; 56( 1): 1-7.[citado 2024 jun. 13 ] Available from: https://dx.doi.org/10.3390/ASEC2023-16272
  • Source: Rapid Prototyping Journal: the international journal for research on additive manufacturing and 3D printing. Unidade: EESC

    Subjects: ALGORITMOS, MANUFATURA ADITIVA, ENGENHARIA MECÂNICA

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      IDOGAVA, Henrique Takashi et al. AltPrint: new filling and slicing process planning based on deposited material with geometry variation. Rapid Prototyping Journal: the international journal for research on additive manufacturing and 3D printing, p. 1-13, 2023Tradução . . Disponível em: https://doi.org/10.1108/RPJ-06-2022-0208. Acesso em: 13 jun. 2024.
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      Idogava, H. T., Couto, D. M. S. do, Santana, L., Alves, J. L., & Silveira, Z. de C. (2023). AltPrint: new filling and slicing process planning based on deposited material with geometry variation. Rapid Prototyping Journal: the international journal for research on additive manufacturing and 3D printing, 1-13. doi:10.1108/RPJ-06-2022-0208
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      Idogava HT, Couto DMS do, Santana L, Alves JL, Silveira Z de C. AltPrint: new filling and slicing process planning based on deposited material with geometry variation [Internet]. Rapid Prototyping Journal: the international journal for research on additive manufacturing and 3D printing. 2023 ; 1-13.[citado 2024 jun. 13 ] Available from: https://doi.org/10.1108/RPJ-06-2022-0208
    • Vancouver

      Idogava HT, Couto DMS do, Santana L, Alves JL, Silveira Z de C. AltPrint: new filling and slicing process planning based on deposited material with geometry variation [Internet]. Rapid Prototyping Journal: the international journal for research on additive manufacturing and 3D printing. 2023 ; 1-13.[citado 2024 jun. 13 ] Available from: https://doi.org/10.1108/RPJ-06-2022-0208
  • Source: Aerospace. Unidade: EESC

    Subjects: AEROFÓLIOS, AEROELASTICIDADE DE AERONAVES, FLAPS, ENGENHARIA MECÂNICA

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      CAMACHO, Emanuel A. R. e MARQUES, Flavio Donizeti e SILVA, Andre R. R. Influence of a deflectable leading-edge on a flapping airfoil. Aerospace, v. 10, n. 7, p. 1-17, 2023Tradução . . Disponível em: https://doi.org/10.3390/aerospace10070615. Acesso em: 13 jun. 2024.
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      Camacho, E. A. R., Marques, F. D., & Silva, A. R. R. (2023). Influence of a deflectable leading-edge on a flapping airfoil. Aerospace, 10( 7), 1-17. doi:10.3390/aerospace10070615
    • NLM

      Camacho EAR, Marques FD, Silva ARR. Influence of a deflectable leading-edge on a flapping airfoil [Internet]. Aerospace. 2023 ; 10( 7): 1-17.[citado 2024 jun. 13 ] Available from: https://doi.org/10.3390/aerospace10070615
    • Vancouver

      Camacho EAR, Marques FD, Silva ARR. Influence of a deflectable leading-edge on a flapping airfoil [Internet]. Aerospace. 2023 ; 10( 7): 1-17.[citado 2024 jun. 13 ] Available from: https://doi.org/10.3390/aerospace10070615
  • Source: Composite Structures. Unidade: EESC

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

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      CABRAL, Myrella Vieira e MARQUES, Flavio Donizeti e FERREIRA, Antonio J. M. Nonlinear supersonic post-flutter response of two-bay composite laminate curved panels. Composite Structures, v. 286, p. 1-15, 2022Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2021.115128. Acesso em: 13 jun. 2024.
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      Cabral, M. V., Marques, F. D., & Ferreira, A. J. M. (2022). Nonlinear supersonic post-flutter response of two-bay composite laminate curved panels. Composite Structures, 286, 1-15. doi:10.1016/j.compstruct.2021.115128
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      Cabral MV, Marques FD, Ferreira AJM. Nonlinear supersonic post-flutter response of two-bay composite laminate curved panels [Internet]. Composite Structures. 2022 ; 286 1-15.[citado 2024 jun. 13 ] Available from: https://doi.org/10.1016/j.compstruct.2021.115128
    • Vancouver

      Cabral MV, Marques FD, Ferreira AJM. Nonlinear supersonic post-flutter response of two-bay composite laminate curved panels [Internet]. Composite Structures. 2022 ; 286 1-15.[citado 2024 jun. 13 ] Available from: https://doi.org/10.1016/j.compstruct.2021.115128
  • Source: Thin-Walled Structures. Unidade: EESC

    Subjects: 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: 13 jun. 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 jun. 13 ] 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 jun. 13 ] Available from: https://doi.org/10.1016/j.tws.2021.108864
  • Source: International Journal of Advanced Manufacturing Technology. Unidade: EESC

    Subjects: MANUFATURA, EXTRUSÃO, TERCEIRA DIMENSÃO, ENGENHARIA MECÂNICA

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      JUSTINO NETTO, Joaquim Manoel et al. Screw-assisted 3D printing with granulated materials: a systematic review. International Journal of Advanced Manufacturing Technology, p. 1-17, 2021Tradução . . Disponível em: https://doi.org/10.1007/s00170-021-07365-z. Acesso em: 13 jun. 2024.
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      Justino Netto, J. M., Idogava, H. T., Santos, L. E. F., Silveira, Z. de C., Romio, P., & Alves, J. L. (2021). Screw-assisted 3D printing with granulated materials: a systematic review. International Journal of Advanced Manufacturing Technology, 1-17. doi:10.1007/s00170-021-07365-z
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      Justino Netto JM, Idogava HT, Santos LEF, Silveira Z de C, Romio P, Alves JL. Screw-assisted 3D printing with granulated materials: a systematic review [Internet]. International Journal of Advanced Manufacturing Technology. 2021 ; 1-17.[citado 2024 jun. 13 ] Available from: https://doi.org/10.1007/s00170-021-07365-z
    • Vancouver

      Justino Netto JM, Idogava HT, Santos LEF, Silveira Z de C, Romio P, Alves JL. Screw-assisted 3D printing with granulated materials: a systematic review [Internet]. International Journal of Advanced Manufacturing Technology. 2021 ; 1-17.[citado 2024 jun. 13 ] Available from: https://doi.org/10.1007/s00170-021-07365-z
  • Source: Thin-Walled Structures. Unidade: EESC

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

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      CABRAL, Myrella V. e MARQUES, Flavio Donizeti e FERREIRA, António J. M. The effect of curvature in nonlinear supersonic flutter of panels with adjacent bays. Thin-Walled Structures, v. 161, p. 1-12, 2021Tradução . . Disponível em: https://doi.org/10.1016/j.tws.2020.107379. Acesso em: 13 jun. 2024.
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      Cabral, M. V., Marques, F. D., & Ferreira, A. J. M. (2021). The effect of curvature in nonlinear supersonic flutter of panels with adjacent bays. Thin-Walled Structures, 161, 1-12. doi:10.1016/j.tws.2020.107379
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      Cabral MV, Marques FD, Ferreira AJM. The effect of curvature in nonlinear supersonic flutter of panels with adjacent bays [Internet]. Thin-Walled Structures. 2021 ; 161 1-12.[citado 2024 jun. 13 ] Available from: https://doi.org/10.1016/j.tws.2020.107379
    • Vancouver

      Cabral MV, Marques FD, Ferreira AJM. The effect of curvature in nonlinear supersonic flutter of panels with adjacent bays [Internet]. Thin-Walled Structures. 2021 ; 161 1-12.[citado 2024 jun. 13 ] Available from: https://doi.org/10.1016/j.tws.2020.107379
  • Source: Latin American Journal of Solids and Structures. Unidade: EESC

    Subjects: ESTRUTURAS DE AÇO, MÉTODO DOS ELEMENTOS FINITOS, ENGENHARIA MECÂNICA

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      MASSAROPPI JÚNIOR, Ernesto et al. Collapse of I-section tapered beam-columns in medium-span steel frames: finite element model validation and parameters influence evaluation. Latin American Journal of Solids and Structures, v. No 2020, n. 8, p. 1-33, 2020Tradução . . Disponível em: https://doi.org/10.1590/1679-78256050. Acesso em: 13 jun. 2024.
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      Massaroppi Júnior, E., Zampaolo, T. C., Abambres, M., & Ribeiro, T. P. (2020). Collapse of I-section tapered beam-columns in medium-span steel frames: finite element model validation and parameters influence evaluation. Latin American Journal of Solids and Structures, No 2020( 8), 1-33. doi:10.1590/1679-78256050
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      Massaroppi Júnior E, Zampaolo TC, Abambres M, Ribeiro TP. Collapse of I-section tapered beam-columns in medium-span steel frames: finite element model validation and parameters influence evaluation [Internet]. Latin American Journal of Solids and Structures. 2020 ; No 2020( 8): 1-33.[citado 2024 jun. 13 ] Available from: https://doi.org/10.1590/1679-78256050
    • Vancouver

      Massaroppi Júnior E, Zampaolo TC, Abambres M, Ribeiro TP. Collapse of I-section tapered beam-columns in medium-span steel frames: finite element model validation and parameters influence evaluation [Internet]. Latin American Journal of Solids and Structures. 2020 ; No 2020( 8): 1-33.[citado 2024 jun. 13 ] Available from: https://doi.org/10.1590/1679-78256050
  • Source: Proceedings. Conference titles: AIAA Scitech Forum. Unidade: EESC

    Subjects: PAINÉIS, AEROELASTICIDADE DE AERONAVES, ENGENHARIA MECÂNICA

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      MARQUES, Flavio Donizeti e FERREIRA, A. J. M. Nonlinear dynamics of fluttering multibay panels in supersonic regime. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-1867. Acesso em: 13 jun. 2024.
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      Marques, F. D., & Ferreira, A. J. M. (2019). Nonlinear dynamics of fluttering multibay panels in supersonic regime. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-1867
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      Marques FD, Ferreira AJM. Nonlinear dynamics of fluttering multibay panels in supersonic regime [Internet]. Proceedings. 2019 ;[citado 2024 jun. 13 ] Available from: https://doi.org/10.2514/6.2019-1867
    • Vancouver

      Marques FD, Ferreira AJM. Nonlinear dynamics of fluttering multibay panels in supersonic regime [Internet]. Proceedings. 2019 ;[citado 2024 jun. 13 ] Available from: https://doi.org/10.2514/6.2019-1867
  • 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: 13 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
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      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. 13 ] 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. 13 ] Available from: https://doi.org/10.1016/j.ijnonlinmec.2018.08.009
  • Source: Proceedings. Conference titles: Iberian Latin-American Congress on Computational Methods in Engineering - CILAMCE. Unidade: EESC

    Subjects: ESTRUTURAS DE AÇO, MÉTODO DOS ELEMENTOS FINITOS, ENGENHARIA MECÂNICA

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      ZAMPAOLO, Tiago César et al. Collapse of parabolically tapered CHS steel columns: finite element model validation. 2018, Anais.. [Belo Horizonte, MG]: ABMEC, 2018. Disponível em: https://repositorio.usp.br/directbitstream/711ab73a-1cac-4aa0-a1c8-94f17baad683/Anais_8-%20Collapse%20of%20parabolically%20tapered%20CHS%20steel%20columns-%20Finite%20element%20model%20validation.pdf. Acesso em: 13 jun. 2024.
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      Zampaolo, T. C., Massaroppi Júnior, E., Abambres, M., & Ribeiro, T. P. (2018). Collapse of parabolically tapered CHS steel columns: finite element model validation. In Proceedings. [Belo Horizonte, MG]: ABMEC. Recuperado de https://repositorio.usp.br/directbitstream/711ab73a-1cac-4aa0-a1c8-94f17baad683/Anais_8-%20Collapse%20of%20parabolically%20tapered%20CHS%20steel%20columns-%20Finite%20element%20model%20validation.pdf
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      Zampaolo TC, Massaroppi Júnior E, Abambres M, Ribeiro TP. Collapse of parabolically tapered CHS steel columns: finite element model validation [Internet]. Proceedings. 2018 ;[citado 2024 jun. 13 ] Available from: https://repositorio.usp.br/directbitstream/711ab73a-1cac-4aa0-a1c8-94f17baad683/Anais_8-%20Collapse%20of%20parabolically%20tapered%20CHS%20steel%20columns-%20Finite%20element%20model%20validation.pdf
    • Vancouver

      Zampaolo TC, Massaroppi Júnior E, Abambres M, Ribeiro TP. Collapse of parabolically tapered CHS steel columns: finite element model validation [Internet]. Proceedings. 2018 ;[citado 2024 jun. 13 ] Available from: https://repositorio.usp.br/directbitstream/711ab73a-1cac-4aa0-a1c8-94f17baad683/Anais_8-%20Collapse%20of%20parabolically%20tapered%20CHS%20steel%20columns-%20Finite%20element%20model%20validation.pdf
  • 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: 13 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
    • NLM

      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. 13 ] 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. 13 ] 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: 13 jun. 2024.
    • APA

      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
    • NLM

      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. 13 ] 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. 13 ] 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: 13 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
    • NLM

      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. 13 ] 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. 13 ] 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: 13 jun. 2024.
    • APA

      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
    • NLM

      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. 13 ] 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. 13 ] Available from: https://doi.org/10.1016/j.tws.2017.08.034
  • Source: Biodegradable polymers : advancement in biodegradation study and applications. Unidade: EESC

    Subjects: POLÍMEROS (MATERIAIS), ENGENHARIA MECÂNICA, PLÁSTICOS BIODEGRADÁVEIS

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      VIEIRA, Andre C. e GUEDES, Rui M. e TITA, Volnei. Constitutive modeling and mechanical behavior prediction of biodegradable polymers during degradation. Biodegradable polymers : advancement in biodegradation study and applications. Tradução . Hauppauge, NY, USA: Nova Publisher, 2015. v. 1. . . Acesso em: 13 jun. 2024.
    • APA

      Vieira, A. C., Guedes, R. M., & Tita, V. (2015). Constitutive modeling and mechanical behavior prediction of biodegradable polymers during degradation. In Biodegradable polymers : advancement in biodegradation study and applications (Vol. 1). Hauppauge, NY, USA: Nova Publisher.
    • NLM

      Vieira AC, Guedes RM, Tita V. Constitutive modeling and mechanical behavior prediction of biodegradable polymers during degradation. In: Biodegradable polymers : advancement in biodegradation study and applications. Hauppauge, NY, USA: Nova Publisher; 2015. [citado 2024 jun. 13 ]
    • Vancouver

      Vieira AC, Guedes RM, Tita V. Constitutive modeling and mechanical behavior prediction of biodegradable polymers during degradation. In: Biodegradable polymers : advancement in biodegradation study and applications. Hauppauge, NY, USA: Nova Publisher; 2015. [citado 2024 jun. 13 ]

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