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  • Fonte: Journal of Aircraft. Unidade: EESC

    Assuntos: AERODINÂMICA DE AERONAVES, AEROELASTICIDADE DE AERONAVES, ENGENHARIA MECÂNICA

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    • ABNT

      SANTOS, João P. T. P. e MARQUES, Flavio Donizeti e BEGNINI, Guilherme R. Influence of nonlinear static deformation on the pre-pazy and pazy wing flutter. Journal of Aircraft, v. 62, n. Ja/Feb. 2025, p. 146-165, 2025Tradução . . Disponível em: http://dx.doi.org/10.2514/1.C037820. Acesso em: 24 nov. 2025.
    • APA

      Santos, J. P. T. P., Marques, F. D., & Begnini, G. R. (2025). Influence of nonlinear static deformation on the pre-pazy and pazy wing flutter. Journal of Aircraft, 62( Ja/Feb. 2025), 146-165. doi:10.2514/1.C037820
    • NLM

      Santos JPTP, Marques FD, Begnini GR. Influence of nonlinear static deformation on the pre-pazy and pazy wing flutter [Internet]. Journal of Aircraft. 2025 ; 62( Ja/Feb. 2025): 146-165.[citado 2025 nov. 24 ] Available from: http://dx.doi.org/10.2514/1.C037820
    • Vancouver

      Santos JPTP, Marques FD, Begnini GR. Influence of nonlinear static deformation on the pre-pazy and pazy wing flutter [Internet]. Journal of Aircraft. 2025 ; 62( Ja/Feb. 2025): 146-165.[citado 2025 nov. 24 ] Available from: http://dx.doi.org/10.2514/1.C037820
  • Fonte: Journal of Aircraft. Unidade: EESC

    Assuntos: DINÂMICA DE VOO, AERODINÂMICA DE AERONAVES, ENGENHARIA MECÂNICA

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    • ABNT

      SANTOS, Carlos Renan dos e MARQUES, Flavio Donizeti. Lift prediction including stall, using vortex lattice method with Kirchhoff-Based correction. Journal of Aircraft, v. 55, n. 2, p. 887-891, 2018Tradução . . Disponível em: https://doi.org/10.2514/1.C034451. Acesso em: 24 nov. 2025.
    • APA

      Santos, C. R. dos, & Marques, F. D. (2018). Lift prediction including stall, using vortex lattice method with Kirchhoff-Based correction. Journal of Aircraft, 55( 2), 887-891. doi:10.2514/1.C034451
    • NLM

      Santos CR dos, Marques FD. Lift prediction including stall, using vortex lattice method with Kirchhoff-Based correction [Internet]. Journal of Aircraft. 2018 ; 55( 2): 887-891.[citado 2025 nov. 24 ] Available from: https://doi.org/10.2514/1.C034451
    • Vancouver

      Santos CR dos, Marques FD. Lift prediction including stall, using vortex lattice method with Kirchhoff-Based correction [Internet]. Journal of Aircraft. 2018 ; 55( 2): 887-891.[citado 2025 nov. 24 ] Available from: https://doi.org/10.2514/1.C034451
  • Fonte: Journal of Aircraft. Unidade: EESC

    Assuntos: TÚNEIS DE VENTO (TESTES), ASAS DE AERONAVES

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    • ABNT

      CERÓN MUÑOZ, Hernán Darío et al. Experimental investigation of wing-tip devices on the reduction of induced drag. Journal of Aircraft, v. 50, n. 2, p. 441-449, 2013Tradução . . Disponível em: https://doi.org/10.2514/1.C031862. Acesso em: 24 nov. 2025.
    • APA

      Cerón Muñoz, H. D., Cosin, R., Coimbra, R. F. de F., Correa, L. G. N., & Catalano, F. M. (2013). Experimental investigation of wing-tip devices on the reduction of induced drag. Journal of Aircraft, 50( 2), 441-449. doi:10.2514/1.C031862
    • NLM

      Cerón Muñoz HD, Cosin R, Coimbra RF de F, Correa LGN, Catalano FM. Experimental investigation of wing-tip devices on the reduction of induced drag [Internet]. Journal of Aircraft. 2013 ; 50( 2): 441-449.[citado 2025 nov. 24 ] Available from: https://doi.org/10.2514/1.C031862
    • Vancouver

      Cerón Muñoz HD, Cosin R, Coimbra RF de F, Correa LGN, Catalano FM. Experimental investigation of wing-tip devices on the reduction of induced drag [Internet]. Journal of Aircraft. 2013 ; 50( 2): 441-449.[citado 2025 nov. 24 ] Available from: https://doi.org/10.2514/1.C031862
  • Fonte: Journal of Aircraft. Unidade: EP

    Assuntos: EFEITOS DO CALOR NA MATÉRIA, AERODINÂMICA DE AERONAVES, MODELOS MATEMÁTICOS, TERMODINÂMICA

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    • ABNT

      SILVA, Guilherme Araújo Lima da e ZERBINI, Euryale Jorge Godoy de Jesus. Numerical simulation of airfoil thermal anti-ice operation Part 1: Mathematical modeling. Journal of Aircraft, v. 44, n. 2, p. 627-634, 2006Tradução . . Disponível em: https://repositorio.usp.br/directbitstream/7ca83da4-8d2e-4240-9f58-c9e146081256/Silvares-2006-Numerical%20Simulation%20of%20Airfoil%20Thermal%20Anti-ice%20Operation%2C%20Part%201_%20Mathematical%20Modelling.pdf. Acesso em: 24 nov. 2025.
    • APA

      Silva, G. A. L. da, & Zerbini, E. J. G. de J. (2006). Numerical simulation of airfoil thermal anti-ice operation Part 1: Mathematical modeling. Journal of Aircraft, 44( 2), 627-634. Recuperado de https://repositorio.usp.br/directbitstream/7ca83da4-8d2e-4240-9f58-c9e146081256/Silvares-2006-Numerical%20Simulation%20of%20Airfoil%20Thermal%20Anti-ice%20Operation%2C%20Part%201_%20Mathematical%20Modelling.pdf
    • NLM

      Silva GAL da, Zerbini EJG de J. Numerical simulation of airfoil thermal anti-ice operation Part 1: Mathematical modeling [Internet]. Journal of Aircraft. 2006 ;44( 2): 627-634.[citado 2025 nov. 24 ] Available from: https://repositorio.usp.br/directbitstream/7ca83da4-8d2e-4240-9f58-c9e146081256/Silvares-2006-Numerical%20Simulation%20of%20Airfoil%20Thermal%20Anti-ice%20Operation%2C%20Part%201_%20Mathematical%20Modelling.pdf
    • Vancouver

      Silva GAL da, Zerbini EJG de J. Numerical simulation of airfoil thermal anti-ice operation Part 1: Mathematical modeling [Internet]. Journal of Aircraft. 2006 ;44( 2): 627-634.[citado 2025 nov. 24 ] Available from: https://repositorio.usp.br/directbitstream/7ca83da4-8d2e-4240-9f58-c9e146081256/Silvares-2006-Numerical%20Simulation%20of%20Airfoil%20Thermal%20Anti-ice%20Operation%2C%20Part%201_%20Mathematical%20Modelling.pdf
  • Fonte: Journal of Aircraft. Unidade: EP

    Assuntos: EFEITOS DO CALOR NA MATÉRIA, AERODINÂMICA DE AERONAVES, MODELOS MATEMÁTICOS, TRANSFERÊNCIA DE CALOR

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    • ABNT

      SILVA, Guilherme Araújo Lima da e ZERBINI, Euryale Jorge Godoy de Jesus. Numerical simulation of airfoil thermal anti-ice operation Part 2: implementation and results. Journal of Aircraft, v. 44, n. 2, p. 635-641, 2006Tradução . . Disponível em: https://repositorio.usp.br/directbitstream/fc8aef8f-b99a-41ad-a63b-e78a432d8f30/Silvares-2006-Numerical%20Simulation%20of%20Airfoil%20Thermal%20Anti-ice%20Operation%2C%20Part%202_Implementation%20and%20Results.pdf. Acesso em: 24 nov. 2025.
    • APA

      Silva, G. A. L. da, & Zerbini, E. J. G. de J. (2006). Numerical simulation of airfoil thermal anti-ice operation Part 2: implementation and results. Journal of Aircraft, 44( 2), 635-641. Recuperado de https://repositorio.usp.br/directbitstream/fc8aef8f-b99a-41ad-a63b-e78a432d8f30/Silvares-2006-Numerical%20Simulation%20of%20Airfoil%20Thermal%20Anti-ice%20Operation%2C%20Part%202_Implementation%20and%20Results.pdf
    • NLM

      Silva GAL da, Zerbini EJG de J. Numerical simulation of airfoil thermal anti-ice operation Part 2: implementation and results [Internet]. Journal of Aircraft. 2006 ;44( 2): 635-641.[citado 2025 nov. 24 ] Available from: https://repositorio.usp.br/directbitstream/fc8aef8f-b99a-41ad-a63b-e78a432d8f30/Silvares-2006-Numerical%20Simulation%20of%20Airfoil%20Thermal%20Anti-ice%20Operation%2C%20Part%202_Implementation%20and%20Results.pdf
    • Vancouver

      Silva GAL da, Zerbini EJG de J. Numerical simulation of airfoil thermal anti-ice operation Part 2: implementation and results [Internet]. Journal of Aircraft. 2006 ;44( 2): 635-641.[citado 2025 nov. 24 ] Available from: https://repositorio.usp.br/directbitstream/fc8aef8f-b99a-41ad-a63b-e78a432d8f30/Silvares-2006-Numerical%20Simulation%20of%20Airfoil%20Thermal%20Anti-ice%20Operation%2C%20Part%202_Implementation%20and%20Results.pdf

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