Filtros : "ENGENHARIA AERONÁUTICA" "2017" Limpar

Filtros



Refine with date range


  • Source: Proceedings of MECSOL. Conference titles: International Symposium on Solid Mechanics - MECSOL. Unidade: EESC

    Subjects: MÉTODO DOS ELEMENTOS FINITOS, FRATURA DAS ESTRUTURAS, JUNTAS ESTRUTURAIS, ENGENHARIA AERONÁUTICA

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

      ANGELO, Marcus Vinícius e RIBEIRO, Marcelo Leite e TITA, Volnei. Action plane fracture criterion applied to extended finite method: a framework for onset and crack propagation. 2017, Anais.. Joinville, SC: Escola de Engenharia de São Carlos, Universidade de São Paulo, 2017. . Acesso em: 27 nov. 2025.
    • APA

      Angelo, M. V., Ribeiro, M. L., & Tita, V. (2017). Action plane fracture criterion applied to extended finite method: a framework for onset and crack propagation. In Proceedings of MECSOL. Joinville, SC: Escola de Engenharia de São Carlos, Universidade de São Paulo.
    • NLM

      Angelo MV, Ribeiro ML, Tita V. Action plane fracture criterion applied to extended finite method: a framework for onset and crack propagation. Proceedings of MECSOL. 2017 ;[citado 2025 nov. 27 ]
    • Vancouver

      Angelo MV, Ribeiro ML, Tita V. Action plane fracture criterion applied to extended finite method: a framework for onset and crack propagation. Proceedings of MECSOL. 2017 ;[citado 2025 nov. 27 ]
  • Source: Journal of Fluid Mechanics. Unidade: EESC

    Subjects: RUGOSIDADE SUPERFICIAL, ENGENHARIA AERONÁUTICA

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

      PAULA, I. B. de et al. Interaction of instability waves and a three-dimensional roughness element in a boundary layer. Journal of Fluid Mechanics, v. 824, p. 624-660, 2017Tradução . . Disponível em: https://doi.org/10.1017/jfm.2017.362. Acesso em: 27 nov. 2025.
    • APA

      Paula, I. B. de, Würz, W., Mendonça, M. T., & Medeiros, M. A. F. de. (2017). Interaction of instability waves and a three-dimensional roughness element in a boundary layer. Journal of Fluid Mechanics, 824, 624-660. doi:10.1017/jfm.2017.362
    • NLM

      Paula IB de, Würz W, Mendonça MT, Medeiros MAF de. Interaction of instability waves and a three-dimensional roughness element in a boundary layer [Internet]. Journal of Fluid Mechanics. 2017 ; 824 624-660.[citado 2025 nov. 27 ] Available from: https://doi.org/10.1017/jfm.2017.362
    • Vancouver

      Paula IB de, Würz W, Mendonça MT, Medeiros MAF de. Interaction of instability waves and a three-dimensional roughness element in a boundary layer [Internet]. Journal of Fluid Mechanics. 2017 ; 824 624-660.[citado 2025 nov. 27 ] Available from: https://doi.org/10.1017/jfm.2017.362
  • Source: Journal of Sound and Vibration. Unidade: EESC

    Subjects: PIEZOELETRICIDADE, AEROELASTICIDADE DE AERONAVES, ENGENHARIA AERONÁUTICA

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

      SOUSA, Vagner Candido de e SILVA, Tarcísio Marinelli Pereira e DE MARQUI JÚNIOR, Carlos. Aeroelastic flutter enhancement by exploiting the combined use of shape memory alloys and nonlinear piezoelectric circuits. Journal of Sound and Vibration, v. 407, p. 46-62, 2017Tradução . . Disponível em: https://doi.org/10.1016/j.jsv.2017.06.034. Acesso em: 27 nov. 2025.
    • APA

      Sousa, V. C. de, Silva, T. M. P., & De Marqui Júnior, C. (2017). Aeroelastic flutter enhancement by exploiting the combined use of shape memory alloys and nonlinear piezoelectric circuits. Journal of Sound and Vibration, 407, 46-62. doi:10.1016/j.jsv.2017.06.034
    • NLM

      Sousa VC de, Silva TMP, De Marqui Júnior C. Aeroelastic flutter enhancement by exploiting the combined use of shape memory alloys and nonlinear piezoelectric circuits [Internet]. Journal of Sound and Vibration. 2017 ; 407 46-62.[citado 2025 nov. 27 ] Available from: https://doi.org/10.1016/j.jsv.2017.06.034
    • Vancouver

      Sousa VC de, Silva TMP, De Marqui Júnior C. Aeroelastic flutter enhancement by exploiting the combined use of shape memory alloys and nonlinear piezoelectric circuits [Internet]. Journal of Sound and Vibration. 2017 ; 407 46-62.[citado 2025 nov. 27 ] Available from: https://doi.org/10.1016/j.jsv.2017.06.034
  • Source: Applied Mathematical Modelling. Unidade: EESC

    Subjects: AEROELASTICIDADE DE AERONAVES, MOLAS HELICOIDAIS, ENGENHARIA AERONÁUTICA

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

      SOUSA, Vagner Candido de e DE MARQUI JÚNIOR, Carlos e ELAHINIA, Mohammad H. Aeroelastic behavior of a typical section with shape memory alloy springs: modeling nonhomogeneous distribution of state variables. Applied Mathematical Modelling, v. 52, p. 404-416, 2017Tradução . . Disponível em: https://doi.org/10.1016/j.apm.2017.07.056. Acesso em: 27 nov. 2025.
    • APA

      Sousa, V. C. de, De Marqui Júnior, C., & Elahinia, M. H. (2017). Aeroelastic behavior of a typical section with shape memory alloy springs: modeling nonhomogeneous distribution of state variables. Applied Mathematical Modelling, 52, 404-416. doi:10.1016/j.apm.2017.07.056
    • NLM

      Sousa VC de, De Marqui Júnior C, Elahinia MH. Aeroelastic behavior of a typical section with shape memory alloy springs: modeling nonhomogeneous distribution of state variables [Internet]. Applied Mathematical Modelling. 2017 ; 52 404-416.[citado 2025 nov. 27 ] Available from: https://doi.org/10.1016/j.apm.2017.07.056
    • Vancouver

      Sousa VC de, De Marqui Júnior C, Elahinia MH. Aeroelastic behavior of a typical section with shape memory alloy springs: modeling nonhomogeneous distribution of state variables [Internet]. Applied Mathematical Modelling. 2017 ; 52 404-416.[citado 2025 nov. 27 ] Available from: https://doi.org/10.1016/j.apm.2017.07.056
  • 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: 27 nov. 2025.
    • 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 2025 nov. 27 ] 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 2025 nov. 27 ] Available from: https://doi.org/10.1016/j.compstruct.2017.07.054
  • Source: Anais. Conference titles: Meeting on Aeronautical Composite Materials and Structures - MACMS 2015. Unidade: EESC

    Subjects: LAMINADOS, ENGENHARIA AERONÁUTICA

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

      AGUIAR, Adair Roberto e PRADO, Edmar Borges Theóphilo. An investigation of material stability in periodic two-phase and hyperelastic laminates. 2017, Anais.. São Carlos, SP: EESC-USP, 2017. Disponível em: http://soac.eesc.usp.br/index.php/macms/macms/paper/view/311/282. Acesso em: 27 nov. 2025.
    • APA

      Aguiar, A. R., & Prado, E. B. T. (2017). An investigation of material stability in periodic two-phase and hyperelastic laminates. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/macms/macms/paper/view/311/282
    • NLM

      Aguiar AR, Prado EBT. An investigation of material stability in periodic two-phase and hyperelastic laminates [Internet]. Anais. 2017 ;[citado 2025 nov. 27 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms/paper/view/311/282
    • Vancouver

      Aguiar AR, Prado EBT. An investigation of material stability in periodic two-phase and hyperelastic laminates [Internet]. Anais. 2017 ;[citado 2025 nov. 27 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms/paper/view/311/282
  • Source: Anais. Conference titles: Meeting on Aeronautical Composite Materials and Structures - MACMS 2015. Unidade: EESC

    Subjects: MÉTODO DOS ELEMENTOS FINITOS, ESTRUTURA DE AERONAVES, ENGENHARIA AERONÁUTICA

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

      CALIRI JR., Mauricio F. e FERREIRA, Antonio J. M. e TITA, Volnei. The use of legendre polynomials on plate theories. 2017, Anais.. São Carlos, SP: EESC-USP, 2017. Disponível em: http://soac.eesc.usp.br/index.php/macms/macms/paper/view/319/257. Acesso em: 27 nov. 2025.
    • APA

      Caliri Jr., M. F., Ferreira, A. J. M., & Tita, V. (2017). The use of legendre polynomials on plate theories. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/macms/macms/paper/view/319/257
    • NLM

      Caliri Jr. MF, Ferreira AJM, Tita V. The use of legendre polynomials on plate theories [Internet]. Anais. 2017 ;[citado 2025 nov. 27 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms/paper/view/319/257
    • Vancouver

      Caliri Jr. MF, Ferreira AJM, Tita V. The use of legendre polynomials on plate theories [Internet]. Anais. 2017 ;[citado 2025 nov. 27 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms/paper/view/319/257
  • Source: Anais. Conference titles: Meeting on Aeronautical Composite Materials and Structures - MACMS 2015. Unidade: EESC

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

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

      FERREIRA, G. F. O. e TITA, Volnei. Evaluation of a material model considering a fiber progressive damage behavior. 2017, Anais.. São Carlos, SP: EESC-USP, 2017. Disponível em: http://soac.eesc.usp.br/index.php/macms/macms/paper/view/312/251. Acesso em: 27 nov. 2025.
    • APA

      Ferreira, G. F. O., & Tita, V. (2017). Evaluation of a material model considering a fiber progressive damage behavior. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/macms/macms/paper/view/312/251
    • NLM

      Ferreira GFO, Tita V. Evaluation of a material model considering a fiber progressive damage behavior [Internet]. Anais. 2017 ;[citado 2025 nov. 27 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms/paper/view/312/251
    • Vancouver

      Ferreira GFO, Tita V. Evaluation of a material model considering a fiber progressive damage behavior [Internet]. Anais. 2017 ;[citado 2025 nov. 27 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms/paper/view/312/251
  • Source: Anais. Conference titles: Meeting on Aeronautical Composite Materials and Structures - MACMS 2017. Unidade: EESC

    Subjects: PIEZOELETRICIDADE, MATERIAIS COMPÓSITOS, HOMOGENEIZAÇÃO, ENGENHARIA AERONÁUTICA

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

      SANTANA, Humberto Brito et al. Effective coefficients for piezoelectric composites with uniform mechanical and electrical imperfect contacts. 2017, Anais.. São Carlos, SP: EESC-USP, 2017. Disponível em: http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/805/527. Acesso em: 27 nov. 2025.
    • APA

      Santana, H. B., Rodríguez Ramos, R., López Realpozo, J. C., Quintero, A. J., Guinovart Diaz, R., Camacho Montes, H., et al. (2017). Effective coefficients for piezoelectric composites with uniform mechanical and electrical imperfect contacts. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/805/527
    • NLM

      Santana HB, Rodríguez Ramos R, López Realpozo JC, Quintero AJ, Guinovart Diaz R, Camacho Montes H, Espinosa Almeyda Y, Sabina FJ, Bravo-Castillero J, Ferreira AJM, Tita V. Effective coefficients for piezoelectric composites with uniform mechanical and electrical imperfect contacts [Internet]. Anais. 2017 ;[citado 2025 nov. 27 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/805/527
    • Vancouver

      Santana HB, Rodríguez Ramos R, López Realpozo JC, Quintero AJ, Guinovart Diaz R, Camacho Montes H, Espinosa Almeyda Y, Sabina FJ, Bravo-Castillero J, Ferreira AJM, Tita V. Effective coefficients for piezoelectric composites with uniform mechanical and electrical imperfect contacts [Internet]. Anais. 2017 ;[citado 2025 nov. 27 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/805/527
  • Source: Anais. Conference titles: Meeting on Aeronautical Composite Materials and Structures - MACMS 2015. Unidade: EESC

    Subjects: MATERIAIS COMPÓSITOS DE FIBRAS CONTÍNUAS, POLÍMEROS (MATERIAIS), ENGENHARIA AERONÁUTICA

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

      BUITRAGO URIBE, Braian Esneider et al. Hierarchical carbon fiber composites with microfibrillated cellulose as secondary reinforcement. 2017, Anais.. São Carlos, SP: EESC-USP, 2017. Disponível em: http://soac.eesc.usp.br/index.php/macms/macms/paper/view/321/259. Acesso em: 27 nov. 2025.
    • APA

      Buitrago Uribe, B. E., Chiromito, E. M. S., Carvalho, A. J. F., & Tarpani, J. R. (2017). Hierarchical carbon fiber composites with microfibrillated cellulose as secondary reinforcement. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/macms/macms/paper/view/321/259
    • NLM

      Buitrago Uribe BE, Chiromito EMS, Carvalho AJF, Tarpani JR. Hierarchical carbon fiber composites with microfibrillated cellulose as secondary reinforcement [Internet]. Anais. 2017 ;[citado 2025 nov. 27 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms/paper/view/321/259
    • Vancouver

      Buitrago Uribe BE, Chiromito EMS, Carvalho AJF, Tarpani JR. Hierarchical carbon fiber composites with microfibrillated cellulose as secondary reinforcement [Internet]. Anais. 2017 ;[citado 2025 nov. 27 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms/paper/view/321/259
  • Source: Anais. Conference titles: Meeting on Aeronautical Composite Materials and Structures - MACMS 2017. Unidade: EESC

    Subjects: MECÂNICA DA FRATURA, MÉTODO DOS ELEMENTOS FINITOS, ESTRUTURA DE AERONAVES, ENGENHARIA AERONÁUTICA

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

      SILVA, Jailto Antonio Prado da et al. Failure analysis of an al 2024-t3 plate using fracture mechanics. 2017, Anais.. São Carlos, SP: EESC-USP, 2017. Disponível em: http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/827/536. Acesso em: 27 nov. 2025.
    • APA

      Silva, J. A. P. da, Aveiga, D., Ribeiro, M. L., Leonel, E. D., Ferreira, A. J. M., & Tita, V. (2017). Failure analysis of an al 2024-t3 plate using fracture mechanics. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/827/536
    • NLM

      Silva JAP da, Aveiga D, Ribeiro ML, Leonel ED, Ferreira AJM, Tita V. Failure analysis of an al 2024-t3 plate using fracture mechanics [Internet]. Anais. 2017 ;[citado 2025 nov. 27 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/827/536
    • Vancouver

      Silva JAP da, Aveiga D, Ribeiro ML, Leonel ED, Ferreira AJM, Tita V. Failure analysis of an al 2024-t3 plate using fracture mechanics [Internet]. Anais. 2017 ;[citado 2025 nov. 27 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/827/536
  • Source: Anais. Conference titles: Meeting on Aeronautical Composite Materials and Structures - MACMS 2017. Unidade: EESC

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

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

      CHRISTOFF, Bruno Guilherme et al. Unidiretional fiber-reinforced composites: an analysis of the influence of an imperfect adhesion on the effective properties. 2017, Anais.. São Carlos, SP: EESC-USP, 2017. Disponível em: http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/1014/545. Acesso em: 27 nov. 2025.
    • APA

      Christoff, B. G., Santana, H. B., Ferreira, A. J. M., & Tita, V. (2017). Unidiretional fiber-reinforced composites: an analysis of the influence of an imperfect adhesion on the effective properties. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/1014/545
    • NLM

      Christoff BG, Santana HB, Ferreira AJM, Tita V. Unidiretional fiber-reinforced composites: an analysis of the influence of an imperfect adhesion on the effective properties [Internet]. Anais. 2017 ;[citado 2025 nov. 27 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/1014/545
    • Vancouver

      Christoff BG, Santana HB, Ferreira AJM, Tita V. Unidiretional fiber-reinforced composites: an analysis of the influence of an imperfect adhesion on the effective properties [Internet]. Anais. 2017 ;[citado 2025 nov. 27 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/1014/545
  • Source: Anais. Conference titles: Meeting on Aeronautical Composite Materials and Structures - MACMS 2017. Unidade: EESC

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

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

      MARQUES, Denys e FERREIRA, António Joaquim Mendes e TITA, Volnei. Structural health monitoring of thin thermoplastic composite plates via vibration based method. 2017, Anais.. São Carlos, SP: EESC-USP, 2017. Disponível em: http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/814/543. Acesso em: 27 nov. 2025.
    • APA

      Marques, D., Ferreira, A. J. M., & Tita, V. (2017). Structural health monitoring of thin thermoplastic composite plates via vibration based method. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/814/543
    • NLM

      Marques D, Ferreira AJM, Tita V. Structural health monitoring of thin thermoplastic composite plates via vibration based method [Internet]. Anais. 2017 ;[citado 2025 nov. 27 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/814/543
    • Vancouver

      Marques D, Ferreira AJM, Tita V. Structural health monitoring of thin thermoplastic composite plates via vibration based method [Internet]. Anais. 2017 ;[citado 2025 nov. 27 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms2017/paper/view/814/543
  • Conference titles: ABCM International Congress of Mechanical Engineering - COBEM. Unidade: EESC

    Subjects: MATERIAIS COMPÓSITOS, ESTRUTURA DE AERONAVES, ENGENHARIA AERONÁUTICA

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

      JARAMILLO BUSTAMANTE, Luis Eduardo et al. A numerical study on the effect of PLY orientation in lamb wave propagation through carbon fiber reinforced composites. 2017, Anais.. Rio de Janeiro, RJ: ABCM, 2017. Disponível em: https://repositorio.usp.br/directbitstream/4febf50a-5f12-41fe-ad14-3e356ed7204b/trabalho%2027%20-%20%20A%20NUMERICAL%20STUDY%20ON%20THE%20EFFECT%20OF%20PLY%20ORIENTATION%20IN%20LAMB%20WAVE%20PROPAGATION%20THROUGH%20CARBON%20FIBER%20REINFORCED%20COMPOSITES%20%28COBEM%202017%29_removed.pdf. Acesso em: 27 nov. 2025.
    • APA

      Jaramillo Bustamante, L. E., Santana, H. B., Tita, V., & Ribeiro, M. L. (2017). A numerical study on the effect of PLY orientation in lamb wave propagation through carbon fiber reinforced composites. In . Rio de Janeiro, RJ: ABCM. Recuperado de https://repositorio.usp.br/directbitstream/4febf50a-5f12-41fe-ad14-3e356ed7204b/trabalho%2027%20-%20%20A%20NUMERICAL%20STUDY%20ON%20THE%20EFFECT%20OF%20PLY%20ORIENTATION%20IN%20LAMB%20WAVE%20PROPAGATION%20THROUGH%20CARBON%20FIBER%20REINFORCED%20COMPOSITES%20%28COBEM%202017%29_removed.pdf
    • NLM

      Jaramillo Bustamante LE, Santana HB, Tita V, Ribeiro ML. A numerical study on the effect of PLY orientation in lamb wave propagation through carbon fiber reinforced composites [Internet]. 2017 ;[citado 2025 nov. 27 ] Available from: https://repositorio.usp.br/directbitstream/4febf50a-5f12-41fe-ad14-3e356ed7204b/trabalho%2027%20-%20%20A%20NUMERICAL%20STUDY%20ON%20THE%20EFFECT%20OF%20PLY%20ORIENTATION%20IN%20LAMB%20WAVE%20PROPAGATION%20THROUGH%20CARBON%20FIBER%20REINFORCED%20COMPOSITES%20%28COBEM%202017%29_removed.pdf
    • Vancouver

      Jaramillo Bustamante LE, Santana HB, Tita V, Ribeiro ML. A numerical study on the effect of PLY orientation in lamb wave propagation through carbon fiber reinforced composites [Internet]. 2017 ;[citado 2025 nov. 27 ] Available from: https://repositorio.usp.br/directbitstream/4febf50a-5f12-41fe-ad14-3e356ed7204b/trabalho%2027%20-%20%20A%20NUMERICAL%20STUDY%20ON%20THE%20EFFECT%20OF%20PLY%20ORIENTATION%20IN%20LAMB%20WAVE%20PROPAGATION%20THROUGH%20CARBON%20FIBER%20REINFORCED%20COMPOSITES%20%28COBEM%202017%29_removed.pdf
  • Source: Anais. Conference titles: International Congress of Mechanical Engineering - COBEM. Unidade: EESC

    Subjects: AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA

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

      LIORBANO, Felipe Fernandes e PELEGRINELI, Luis Antonio Vieira e ANGÉLICO, Ricardo Afonso. Application of Galerkin method to the solution of aerodynamic models based on the lifting-line theory. 2017, Anais.. Rio de Janeiro, RJ: ABCM, 2017. Disponível em: https://repositorio.usp.br/directbitstream/2e83d21b-13bd-4fb4-8b76-02198c7ab7eb/trabalho%2007%20-%20%20Application%20of%20Galerkin%20method%20to%20the%20solution%20of%20aerodynamic%20models%20based%20on%20the%20lifting-line%20theory%20%28COBEM%202017%29.pdf. Acesso em: 27 nov. 2025.
    • APA

      Liorbano, F. F., Pelegrineli, L. A. V., & Angélico, R. A. (2017). Application of Galerkin method to the solution of aerodynamic models based on the lifting-line theory. In Anais. Rio de Janeiro, RJ: ABCM. Recuperado de https://repositorio.usp.br/directbitstream/2e83d21b-13bd-4fb4-8b76-02198c7ab7eb/trabalho%2007%20-%20%20Application%20of%20Galerkin%20method%20to%20the%20solution%20of%20aerodynamic%20models%20based%20on%20the%20lifting-line%20theory%20%28COBEM%202017%29.pdf
    • NLM

      Liorbano FF, Pelegrineli LAV, Angélico RA. Application of Galerkin method to the solution of aerodynamic models based on the lifting-line theory [Internet]. Anais. 2017 ;[citado 2025 nov. 27 ] Available from: https://repositorio.usp.br/directbitstream/2e83d21b-13bd-4fb4-8b76-02198c7ab7eb/trabalho%2007%20-%20%20Application%20of%20Galerkin%20method%20to%20the%20solution%20of%20aerodynamic%20models%20based%20on%20the%20lifting-line%20theory%20%28COBEM%202017%29.pdf
    • Vancouver

      Liorbano FF, Pelegrineli LAV, Angélico RA. Application of Galerkin method to the solution of aerodynamic models based on the lifting-line theory [Internet]. Anais. 2017 ;[citado 2025 nov. 27 ] Available from: https://repositorio.usp.br/directbitstream/2e83d21b-13bd-4fb4-8b76-02198c7ab7eb/trabalho%2007%20-%20%20Application%20of%20Galerkin%20method%20to%20the%20solution%20of%20aerodynamic%20models%20based%20on%20the%20lifting-line%20theory%20%28COBEM%202017%29.pdf
  • Source: Proceedings. Conference titles: AAIA Applied Aerodynamics Conference. Unidade: EESC

    Subjects: AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA

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

      JOUANNET, C. et al. Aeordynamic databased of a subscale demonstrator. 2017, Anais.. Reston, VA, USA: AIAA, 2017. Disponível em: https://repositorio.usp.br/directbitstream/38fa39ae-7494-4553-804a-d323744a4cd2/trabalho%2018%20-%20Aeordynamic%20databased%20of%20a%20subscale%20demonstrator.%20%2835th%20AIAA%20Applied%20Aerodynamics%20Conference%2C%202017%29.pdf. Acesso em: 27 nov. 2025.
    • APA

      Jouannet, C., Lundström, D., Krus, P., Sobron, A., Silva, R. G. A. da, Catalano, F. M., & Greco Júnior, P. C. (2017). Aeordynamic databased of a subscale demonstrator. In Proceedings. Reston, VA, USA: AIAA. Recuperado de https://repositorio.usp.br/directbitstream/38fa39ae-7494-4553-804a-d323744a4cd2/trabalho%2018%20-%20Aeordynamic%20databased%20of%20a%20subscale%20demonstrator.%20%2835th%20AIAA%20Applied%20Aerodynamics%20Conference%2C%202017%29.pdf
    • NLM

      Jouannet C, Lundström D, Krus P, Sobron A, Silva RGA da, Catalano FM, Greco Júnior PC. Aeordynamic databased of a subscale demonstrator [Internet]. Proceedings. 2017 ;[citado 2025 nov. 27 ] Available from: https://repositorio.usp.br/directbitstream/38fa39ae-7494-4553-804a-d323744a4cd2/trabalho%2018%20-%20Aeordynamic%20databased%20of%20a%20subscale%20demonstrator.%20%2835th%20AIAA%20Applied%20Aerodynamics%20Conference%2C%202017%29.pdf
    • Vancouver

      Jouannet C, Lundström D, Krus P, Sobron A, Silva RGA da, Catalano FM, Greco Júnior PC. Aeordynamic databased of a subscale demonstrator [Internet]. Proceedings. 2017 ;[citado 2025 nov. 27 ] Available from: https://repositorio.usp.br/directbitstream/38fa39ae-7494-4553-804a-d323744a4cd2/trabalho%2018%20-%20Aeordynamic%20databased%20of%20a%20subscale%20demonstrator.%20%2835th%20AIAA%20Applied%20Aerodynamics%20Conference%2C%202017%29.pdf
  • Source: Proceedings. Conference titles: Iberian Latin-American Congress on Computational Methods in Engineering - CILAMCE. Unidade: EESC

    Subjects: SLATS, AEROACÚSTICA, ENGENHARIA AERONÁUTICA

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

      HIMENO, Fernando Henrique Tadashi e AMARAL, Filipe Ramos do e MEDEIROS, Marcello Augusto Faraco de. Linear stability theory applied in a cross-stream profile of a shear layer of a leading edge slat. 2017, Anais.. [Belo Horizonte, MG]: ABMEC, 2017. Disponível em: https://repositorio.usp.br/directbitstream/4d9e4862-f0f4-42db-83eb-d4dbf7b966c4/trabalho%2013%20-%20Linear%20Stability%20Theory%20applied%20in%20a%20croos-stream%20profile%20of%20a%20shear%20layer%20of%20leading%20edge%20slat%20%28CILAMCE%202017%29.pdf. Acesso em: 27 nov. 2025.
    • APA

      Himeno, F. H. T., Amaral, F. R. do, & Medeiros, M. A. F. de. (2017). Linear stability theory applied in a cross-stream profile of a shear layer of a leading edge slat. In Proceedings. [Belo Horizonte, MG]: ABMEC. Recuperado de https://repositorio.usp.br/directbitstream/4d9e4862-f0f4-42db-83eb-d4dbf7b966c4/trabalho%2013%20-%20Linear%20Stability%20Theory%20applied%20in%20a%20croos-stream%20profile%20of%20a%20shear%20layer%20of%20leading%20edge%20slat%20%28CILAMCE%202017%29.pdf
    • NLM

      Himeno FHT, Amaral FR do, Medeiros MAF de. Linear stability theory applied in a cross-stream profile of a shear layer of a leading edge slat [Internet]. Proceedings. 2017 ;[citado 2025 nov. 27 ] Available from: https://repositorio.usp.br/directbitstream/4d9e4862-f0f4-42db-83eb-d4dbf7b966c4/trabalho%2013%20-%20Linear%20Stability%20Theory%20applied%20in%20a%20croos-stream%20profile%20of%20a%20shear%20layer%20of%20leading%20edge%20slat%20%28CILAMCE%202017%29.pdf
    • Vancouver

      Himeno FHT, Amaral FR do, Medeiros MAF de. Linear stability theory applied in a cross-stream profile of a shear layer of a leading edge slat [Internet]. Proceedings. 2017 ;[citado 2025 nov. 27 ] Available from: https://repositorio.usp.br/directbitstream/4d9e4862-f0f4-42db-83eb-d4dbf7b966c4/trabalho%2013%20-%20Linear%20Stability%20Theory%20applied%20in%20a%20croos-stream%20profile%20of%20a%20shear%20layer%20of%20leading%20edge%20slat%20%28CILAMCE%202017%29.pdf
  • Source: Proceedings. Conference titles: International Workshop on Structural Health Monitoring. Unidade: EESC

    Subjects: AERONAVES NÃO TRIPULADAS, ROBÓTICA, ASAS DE AERONAVES, ENGENHARIA AERONÁUTICA

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

      ANAYA, Maribel et al. Damage classification based on machine learning applications for an unmanned aerial vehicle. 2017, Anais.. Stanford, CA, USA: Stanford University, 2017. Disponível em: https://repositorio.usp.br/directbitstream/8def7de2-b4c3-4430-81be-eeb78bd1b7ce/trabalho%2012%20-%20Damage%20classification%20based%20on%20machine%20learning%20applications%20for%20an%20unmanned%20aerial%20vehicle%20%28The%2011th%20International%20Workshop%20on%20Structural%20Health%20Monitoring%202017%29.pdf. Acesso em: 27 nov. 2025.
    • APA

      Anaya, M., Cerón Muñoz, H. D., Vitola, J., Tibaduiza, D. A., & Pozo, F. (2017). Damage classification based on machine learning applications for an unmanned aerial vehicle. In Proceedings. Stanford, CA, USA: Stanford University. Recuperado de https://repositorio.usp.br/directbitstream/8def7de2-b4c3-4430-81be-eeb78bd1b7ce/trabalho%2012%20-%20Damage%20classification%20based%20on%20machine%20learning%20applications%20for%20an%20unmanned%20aerial%20vehicle%20%28The%2011th%20International%20Workshop%20on%20Structural%20Health%20Monitoring%202017%29.pdf
    • NLM

      Anaya M, Cerón Muñoz HD, Vitola J, Tibaduiza DA, Pozo F. Damage classification based on machine learning applications for an unmanned aerial vehicle [Internet]. Proceedings. 2017 ;[citado 2025 nov. 27 ] Available from: https://repositorio.usp.br/directbitstream/8def7de2-b4c3-4430-81be-eeb78bd1b7ce/trabalho%2012%20-%20Damage%20classification%20based%20on%20machine%20learning%20applications%20for%20an%20unmanned%20aerial%20vehicle%20%28The%2011th%20International%20Workshop%20on%20Structural%20Health%20Monitoring%202017%29.pdf
    • Vancouver

      Anaya M, Cerón Muñoz HD, Vitola J, Tibaduiza DA, Pozo F. Damage classification based on machine learning applications for an unmanned aerial vehicle [Internet]. Proceedings. 2017 ;[citado 2025 nov. 27 ] Available from: https://repositorio.usp.br/directbitstream/8def7de2-b4c3-4430-81be-eeb78bd1b7ce/trabalho%2012%20-%20Damage%20classification%20based%20on%20machine%20learning%20applications%20for%20an%20unmanned%20aerial%20vehicle%20%28The%2011th%20International%20Workshop%20on%20Structural%20Health%20Monitoring%202017%29.pdf
  • Source: Marine Structures. Unidade: EESC

    Subjects: MÉTODO DOS ELEMENTOS FINITOS, GEOMETRIA E MODELAGEM COMPUTACIONAL, MATERIAIS COMPÓSITOS, ENGENHARIA AERONÁUTICA

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

      TONATTO, Maikson Luiz Passaia et al. Parametric analysis of an offloading hose under internal pressure via computational modeling. Marine Structures, v. 51, n. Ja 2017, p. 174-187, 2017Tradução . . Disponível em: https://doi.org/10.1016/j.marstruc.2016.10.008. Acesso em: 27 nov. 2025.
    • APA

      Tonatto, M. L. P., Tita, V., Araujo, R. T. de, Forte, M. M. C., & Amico, S. C. (2017). Parametric analysis of an offloading hose under internal pressure via computational modeling. Marine Structures, 51( Ja 2017), 174-187. doi:10.1016/j.marstruc.2016.10.008
    • NLM

      Tonatto MLP, Tita V, Araujo RT de, Forte MMC, Amico SC. Parametric analysis of an offloading hose under internal pressure via computational modeling [Internet]. Marine Structures. 2017 ; 51( Ja 2017): 174-187.[citado 2025 nov. 27 ] Available from: https://doi.org/10.1016/j.marstruc.2016.10.008
    • Vancouver

      Tonatto MLP, Tita V, Araujo RT de, Forte MMC, Amico SC. Parametric analysis of an offloading hose under internal pressure via computational modeling [Internet]. Marine Structures. 2017 ; 51( Ja 2017): 174-187.[citado 2025 nov. 27 ] Available from: https://doi.org/10.1016/j.marstruc.2016.10.008
  • Source: Anais. Conference titles: Meeting on Aeronautical Composite Materials and Structures - MACMS 2015. Unidade: EESC

    Subjects: PROCESSOS DE FABRICAÇÃO, MATERIAIS COMPÓSITOS, POLÍMEROS (MATERIAIS), ENGENHARIA AERONÁUTICA

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

      OLIVEIRA, Jeferson de et al. Influence of infrared welding parameters on thermoplastic composite joint quality. 2017, Anais.. São Carlos, SP: EESC-USP, 2017. Disponível em: http://soac.eesc.usp.br/index.php/macms/macms/paper/view/320/280. Acesso em: 27 nov. 2025.
    • APA

      Oliveira, J. de, Bordini, C. C., Angélico, R. A., & Tarpani, J. R. (2017). Influence of infrared welding parameters on thermoplastic composite joint quality. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/macms/macms/paper/view/320/280
    • NLM

      Oliveira J de, Bordini CC, Angélico RA, Tarpani JR. Influence of infrared welding parameters on thermoplastic composite joint quality [Internet]. Anais. 2017 ;[citado 2025 nov. 27 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms/paper/view/320/280
    • Vancouver

      Oliveira J de, Bordini CC, Angélico RA, Tarpani JR. Influence of infrared welding parameters on thermoplastic composite joint quality [Internet]. Anais. 2017 ;[citado 2025 nov. 27 ] Available from: http://soac.eesc.usp.br/index.php/macms/macms/paper/view/320/280

Digital Library of Intellectual Production of Universidade de São Paulo     2012 - 2025