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  • Source: Proceedings. Conference titles: AIAA Scitech Forum. Unidade: IME

    Subjects: DINÂMICA DOS FLUÍDOS, MODELOS MATEMÁTICOS

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      FERRARI, Marcello et al. Accurate CFD measurements of vortex generators effects on a wing subject to shock-induced separation. 2021, Anais.. Reston, VA, USA: AIAA, 2021. Disponível em: https://doi.org/10.2514/6.2021-1839. Acesso em: 05 nov. 2024.
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      Ferrari, M., Morais, K. C., Ferrari, D., Resende, O. C. de, & Santos, L. C. de C. (2021). Accurate CFD measurements of vortex generators effects on a wing subject to shock-induced separation. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2021-1839
    • NLM

      Ferrari M, Morais KC, Ferrari D, Resende OC de, Santos LC de C. Accurate CFD measurements of vortex generators effects on a wing subject to shock-induced separation [Internet]. Proceedings. 2021 ;[citado 2024 nov. 05 ] Available from: https://doi.org/10.2514/6.2021-1839
    • Vancouver

      Ferrari M, Morais KC, Ferrari D, Resende OC de, Santos LC de C. Accurate CFD measurements of vortex generators effects on a wing subject to shock-induced separation [Internet]. Proceedings. 2021 ;[citado 2024 nov. 05 ] Available from: https://doi.org/10.2514/6.2021-1839
  • Source: Proceedings. Conference titles: AIAA Aviation Forum. Unidade: EESC

    Subjects: VOO (ENGENHARIA AERONÁUTICA), ACIDENTES, SIMULADORES DE VOO, ENGENHARIA AERONÁUTICA

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      MACEDO, João Paulo Costa Antunes de e BIDINOTTO, Jorge Henrique e BROMFIELD, Michael A. Loss of control in flight: comparing qualitative pilot opinion with quantitative flight data. 2020, Anais.. Reston, VA, USA: AIAA, 2020. Disponível em: https://doi.org/10.2514/6.2020-2911. Acesso em: 05 nov. 2024.
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      Macedo, J. P. C. A. de, Bidinotto, J. H., & Bromfield, M. A. (2020). Loss of control in flight: comparing qualitative pilot opinion with quantitative flight data. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2020-2911
    • NLM

      Macedo JPCA de, Bidinotto JH, Bromfield MA. Loss of control in flight: comparing qualitative pilot opinion with quantitative flight data [Internet]. Proceedings. 2020 ;[citado 2024 nov. 05 ] Available from: https://doi.org/10.2514/6.2020-2911
    • Vancouver

      Macedo JPCA de, Bidinotto JH, Bromfield MA. Loss of control in flight: comparing qualitative pilot opinion with quantitative flight data [Internet]. Proceedings. 2020 ;[citado 2024 nov. 05 ] Available from: https://doi.org/10.2514/6.2020-2911
  • Source: Proceedings. Conference titles: AIAA Aviation Forum. Unidade: EESC

    Assunto: AEROELASTICIDADE DE AERONAVES

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      VASCONCELLOS, Rui Marcos Grombone de et al. Aeroelastic analysis and characterization of three-degree-of-freedom systems with discontinuous nonlinearity. 2020, Anais.. Reston, VA, USA: AIAA, 2020. Disponível em: https://doi.org/10.2514/6.2020-2665. Acesso em: 05 nov. 2024.
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      Vasconcellos, R. M. G. de, Bouma, A., Marques, F. D., Abdelkefi, A., & Hajj, M. R. (2020). Aeroelastic analysis and characterization of three-degree-of-freedom systems with discontinuous nonlinearity. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2020-2665
    • NLM

      Vasconcellos RMG de, Bouma A, Marques FD, Abdelkefi A, Hajj MR. Aeroelastic analysis and characterization of three-degree-of-freedom systems with discontinuous nonlinearity [Internet]. Proceedings. 2020 ;[citado 2024 nov. 05 ] Available from: https://doi.org/10.2514/6.2020-2665
    • Vancouver

      Vasconcellos RMG de, Bouma A, Marques FD, Abdelkefi A, Hajj MR. Aeroelastic analysis and characterization of three-degree-of-freedom systems with discontinuous nonlinearity [Internet]. Proceedings. 2020 ;[citado 2024 nov. 05 ] Available from: https://doi.org/10.2514/6.2020-2665
  • Source: Proceedings. Conference titles: AIAA Aviation Forum. Unidade: EESC

    Subjects: AEROACÚSTICA, SLATS, ENGENHARIA AERONÁUTICA

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      HIMENO, Fernando Henrique Tadashi et al. Recirculating coherent structures inside the cove of a bulb sealed slat. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-3695. Acesso em: 05 nov. 2024.
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      Himeno, F. H. T., Amaral, F. R. do, Souza, D. S., Rodriguez, D., & Medeiros, M. A. F. de. (2019). Recirculating coherent structures inside the cove of a bulb sealed slat. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-3695
    • NLM

      Himeno FHT, Amaral FR do, Souza DS, Rodriguez D, Medeiros MAF de. Recirculating coherent structures inside the cove of a bulb sealed slat [Internet]. Proceedings. 2019 ;[citado 2024 nov. 05 ] Available from: https://doi.org/10.2514/6.2019-3695
    • Vancouver

      Himeno FHT, Amaral FR do, Souza DS, Rodriguez D, Medeiros MAF de. Recirculating coherent structures inside the cove of a bulb sealed slat [Internet]. Proceedings. 2019 ;[citado 2024 nov. 05 ] Available from: https://doi.org/10.2514/6.2019-3695
  • Source: Proceedings. Conference titles: AIAA Propulsion and Energy Forum. Unidade: EESC

    Subjects: ENGENHARIA AERONÁUTICA, AERODINÂMICA DE AERONAVES

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      BOCCATO, Bruno Ribeiro e BRAVO MOSQUERA, Pedro David e CATALANO, Fernando Martini. Experimental assessment of a non-conventional fighter aircraft: effects of canard on the performance of a dorsal intake. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-4200. Acesso em: 05 nov. 2024.
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      Boccato, B. R., Bravo Mosquera, P. D., & Catalano, F. M. (2019). Experimental assessment of a non-conventional fighter aircraft: effects of canard on the performance of a dorsal intake. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-4200
    • NLM

      Boccato BR, Bravo Mosquera PD, Catalano FM. Experimental assessment of a non-conventional fighter aircraft: effects of canard on the performance of a dorsal intake [Internet]. Proceedings. 2019 ;[citado 2024 nov. 05 ] Available from: https://doi.org/10.2514/6.2019-4200
    • Vancouver

      Boccato BR, Bravo Mosquera PD, Catalano FM. Experimental assessment of a non-conventional fighter aircraft: effects of canard on the performance of a dorsal intake [Internet]. Proceedings. 2019 ;[citado 2024 nov. 05 ] Available from: https://doi.org/10.2514/6.2019-4200
  • 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: 05 nov. 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
    • NLM

      Marques FD, Ferreira AJM. Nonlinear dynamics of fluttering multibay panels in supersonic regime [Internet]. Proceedings. 2019 ;[citado 2024 nov. 05 ] 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 nov. 05 ] Available from: https://doi.org/10.2514/6.2019-1867
  • Source: Proceedings. Conference titles: AIAA Scitech Forum. Unidade: EESC

    Subjects: BIOGRAFIAS, ENGENHARIA MECÂNICA

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      MARQUES, Flavio Donizeti e VASCONCELLOS, Rui Marcos Grombone de. The South Atlantic aerial crossing of João Ribeiro de Barros in 1927. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-1953. Acesso em: 05 nov. 2024.
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      Marques, F. D., & Vasconcellos, R. M. G. de. (2019). The South Atlantic aerial crossing of João Ribeiro de Barros in 1927. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-1953
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      Marques FD, Vasconcellos RMG de. The South Atlantic aerial crossing of João Ribeiro de Barros in 1927 [Internet]. Proceedings. 2019 ;[citado 2024 nov. 05 ] Available from: https://doi.org/10.2514/6.2019-1953
    • Vancouver

      Marques FD, Vasconcellos RMG de. The South Atlantic aerial crossing of João Ribeiro de Barros in 1927 [Internet]. Proceedings. 2019 ;[citado 2024 nov. 05 ] Available from: https://doi.org/10.2514/6.2019-1953
  • Source: Proceedings. Conference titles: AIAA Scitech Forum. Unidade: EESC

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

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      GUIMARÃES, Thiago A. M. et al. Nonlinear multibay panel flutter evaluation of composite laminates with curvilinear fibers. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2020-0941. Acesso em: 05 nov. 2024.
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      Guimarães, T. A. M., Rade, D. A., Cesnik, C. E. S., & Marques, F. D. (2019). Nonlinear multibay panel flutter evaluation of composite laminates with curvilinear fibers. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2020-0941
    • NLM

      Guimarães TAM, Rade DA, Cesnik CES, Marques FD. Nonlinear multibay panel flutter evaluation of composite laminates with curvilinear fibers [Internet]. Proceedings. 2019 ;[citado 2024 nov. 05 ] Available from: https://doi.org/10.2514/6.2020-0941
    • Vancouver

      Guimarães TAM, Rade DA, Cesnik CES, Marques FD. Nonlinear multibay panel flutter evaluation of composite laminates with curvilinear fibers [Internet]. Proceedings. 2019 ;[citado 2024 nov. 05 ] Available from: https://doi.org/10.2514/6.2020-0941
  • Source: Proceedings. Conference titles: AIAA/CEAS Aeroacoustics Conference. Unidade: EESC

    Subjects: ENGENHARIA AERONÁUTICA, AEROACÚSTICA

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      PAGANI JÚNIOR, Carlos do Carmo e CALDAS, Luciano Coutinho e MEDEIROS, Marcello Augusto Faraco de. An experimental and numeric investigation towards a reliable acoustic pressure level estimate using phased-array techniques. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-2700. Acesso em: 05 nov. 2024.
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      Pagani Júnior, C. do C., Caldas, L. C., & Medeiros, M. A. F. de. (2019). An experimental and numeric investigation towards a reliable acoustic pressure level estimate using phased-array techniques. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-2700
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      Pagani Júnior C do C, Caldas LC, Medeiros MAF de. An experimental and numeric investigation towards a reliable acoustic pressure level estimate using phased-array techniques [Internet]. Proceedings. 2019 ;[citado 2024 nov. 05 ] Available from: https://doi.org/10.2514/6.2019-2700
    • Vancouver

      Pagani Júnior C do C, Caldas LC, Medeiros MAF de. An experimental and numeric investigation towards a reliable acoustic pressure level estimate using phased-array techniques [Internet]. Proceedings. 2019 ;[citado 2024 nov. 05 ] Available from: https://doi.org/10.2514/6.2019-2700
  • Source: Proceedings. Conference titles: AIAA/CEAS Aeroacoustics Conference. Unidade: EESC

    Subjects: ENGENHARIA AERONÁUTICA, AEROACÚSTICA, TERCEIRA DIMENSÃO

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      REIS, Danillo Cafaldo dos et al. A study on the 3D effects of slat cove fillers. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-2406. Acesso em: 05 nov. 2024.
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      Reis, D. C. dos, Coelho, E. L. C., Pereira, L. T. L., Catalano, F. M., & Lima, L. S. de M. (2019). A study on the 3D effects of slat cove fillers. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-2406
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      Reis DC dos, Coelho ELC, Pereira LTL, Catalano FM, Lima LS de M. A study on the 3D effects of slat cove fillers [Internet]. Proceedings. 2019 ;[citado 2024 nov. 05 ] Available from: https://doi.org/10.2514/6.2019-2406
    • Vancouver

      Reis DC dos, Coelho ELC, Pereira LTL, Catalano FM, Lima LS de M. A study on the 3D effects of slat cove fillers [Internet]. Proceedings. 2019 ;[citado 2024 nov. 05 ] Available from: https://doi.org/10.2514/6.2019-2406
  • Source: Proceedings. Conference titles: AIAA Propulsion and Energy Forum. Unidade: EESC

    Subjects: ENGENHARIA AERONÁUTICA, ASAS DE AERONAVES, AERODINÂMICA DE AERONAVES

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      BRAVO MOSQUERA, Pedro David e CERÓN MUÑOZ, Hernán Darío e CATALANO, Fernando Martini. Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-3850. Acesso em: 05 nov. 2024.
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      Bravo Mosquera, P. D., Cerón Muñoz, H. D., & Catalano, F. M. (2019). Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-3850
    • NLM

      Bravo Mosquera PD, Cerón Muñoz HD, Catalano FM. Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system [Internet]. Proceedings. 2019 ;[citado 2024 nov. 05 ] Available from: https://doi.org/10.2514/6.2019-3850
    • Vancouver

      Bravo Mosquera PD, Cerón Muñoz HD, Catalano FM. Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system [Internet]. Proceedings. 2019 ;[citado 2024 nov. 05 ] Available from: https://doi.org/10.2514/6.2019-3850
  • Source: Proceedings. Conference titles: AIAA Propulsion and Energy Forum. Unidade: EESC

    Subjects: TRANSFERÊNCIA DE CALOR, AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA

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      RIBEIRO, Daniel Garcia e BRAVO MOSQUERA, Pedro David e CERÓN MUÑOZ, Hernán Darío. Heat transfer effects on aerodynamic performance of a S809 airfoil for wind turbine application. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://repositorio.usp.br/directbitstream/558bdbaf-a0df-406a-aee5-d60273db8fa1/trabalho%2001%20-%20Heat%20transfer%20effects%20on%20aerodynamic%20performance%20of%20a%20S809%20airfoil%20for%20wind%20turbine%20application%20%28AIAA%20Propulsion%20and%20Energy%202019%20Forum%29.pdf. Acesso em: 05 nov. 2024.
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      Ribeiro, D. G., Bravo Mosquera, P. D., & Cerón Muñoz, H. D. (2019). Heat transfer effects on aerodynamic performance of a S809 airfoil for wind turbine application. In Proceedings. Reston, VA, USA: AIAA. Recuperado de https://repositorio.usp.br/directbitstream/558bdbaf-a0df-406a-aee5-d60273db8fa1/trabalho%2001%20-%20Heat%20transfer%20effects%20on%20aerodynamic%20performance%20of%20a%20S809%20airfoil%20for%20wind%20turbine%20application%20%28AIAA%20Propulsion%20and%20Energy%202019%20Forum%29.pdf
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      Ribeiro DG, Bravo Mosquera PD, Cerón Muñoz HD. Heat transfer effects on aerodynamic performance of a S809 airfoil for wind turbine application [Internet]. Proceedings. 2019 ;[citado 2024 nov. 05 ] Available from: https://repositorio.usp.br/directbitstream/558bdbaf-a0df-406a-aee5-d60273db8fa1/trabalho%2001%20-%20Heat%20transfer%20effects%20on%20aerodynamic%20performance%20of%20a%20S809%20airfoil%20for%20wind%20turbine%20application%20%28AIAA%20Propulsion%20and%20Energy%202019%20Forum%29.pdf
    • Vancouver

      Ribeiro DG, Bravo Mosquera PD, Cerón Muñoz HD. Heat transfer effects on aerodynamic performance of a S809 airfoil for wind turbine application [Internet]. Proceedings. 2019 ;[citado 2024 nov. 05 ] Available from: https://repositorio.usp.br/directbitstream/558bdbaf-a0df-406a-aee5-d60273db8fa1/trabalho%2001%20-%20Heat%20transfer%20effects%20on%20aerodynamic%20performance%20of%20a%20S809%20airfoil%20for%20wind%20turbine%20application%20%28AIAA%20Propulsion%20and%20Energy%202019%20Forum%29.pdf
  • Source: AIAA Journal. Unidade: EESC

    Subjects: TÚNEIS DE VENTO, AEROFÓLIOS, ENGENHARIA AERONÁUTICA

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      AMARAL, Filipe Ramos do et al. Effect of bubble seal on slat noise. AIAA Journal, v. 57, n. 4, p. 1-16, 2019Tradução . . Disponível em: https://repositorio.usp.br/directbitstream/476468c6-5ea4-41fd-90ce-a94d619fdc5c/artigo%2004%20-%20Effect%20of%20Bubble%20Seal%20on%20Slat%20Noise%20%28AIAA%20JOURNAL%29.pdf. Acesso em: 05 nov. 2024.
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      Amaral, F. R. do, Himeno, F. H. T., Souza, D. S., & Medeiros, M. A. F. de. (2019). Effect of bubble seal on slat noise. AIAA Journal, 57( 4), 1-16. Recuperado de https://repositorio.usp.br/directbitstream/476468c6-5ea4-41fd-90ce-a94d619fdc5c/artigo%2004%20-%20Effect%20of%20Bubble%20Seal%20on%20Slat%20Noise%20%28AIAA%20JOURNAL%29.pdf
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      Amaral FR do, Himeno FHT, Souza DS, Medeiros MAF de. Effect of bubble seal on slat noise [Internet]. AIAA Journal. 2019 ; 57( 4): 1-16.[citado 2024 nov. 05 ] Available from: https://repositorio.usp.br/directbitstream/476468c6-5ea4-41fd-90ce-a94d619fdc5c/artigo%2004%20-%20Effect%20of%20Bubble%20Seal%20on%20Slat%20Noise%20%28AIAA%20JOURNAL%29.pdf
    • Vancouver

      Amaral FR do, Himeno FHT, Souza DS, Medeiros MAF de. Effect of bubble seal on slat noise [Internet]. AIAA Journal. 2019 ; 57( 4): 1-16.[citado 2024 nov. 05 ] Available from: https://repositorio.usp.br/directbitstream/476468c6-5ea4-41fd-90ce-a94d619fdc5c/artigo%2004%20-%20Effect%20of%20Bubble%20Seal%20on%20Slat%20Noise%20%28AIAA%20JOURNAL%29.pdf
  • Source: Proceedings. Conference titles: AIAA Aviation Forum. Unidade: EESC

    Subjects: AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA

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      MATHIAS, Marlon Sproesser e MEDEIROS, Marcello Augusto Faraco de. Global instability analysis of a boundary layer flow over a small cavity. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-3535. Acesso em: 05 nov. 2024.
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      Mathias, M. S., & Medeiros, M. A. F. de. (2019). Global instability analysis of a boundary layer flow over a small cavity. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-3535
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      Mathias MS, Medeiros MAF de. Global instability analysis of a boundary layer flow over a small cavity [Internet]. Proceedings. 2019 ;[citado 2024 nov. 05 ] Available from: https://doi.org/10.2514/6.2019-3535
    • Vancouver

      Mathias MS, Medeiros MAF de. Global instability analysis of a boundary layer flow over a small cavity [Internet]. Proceedings. 2019 ;[citado 2024 nov. 05 ] Available from: https://doi.org/10.2514/6.2019-3535
  • Source: Proceedings. Conference titles: AIAA/CEAS Aeroacoustics Conference. Unidade: EESC

    Subjects: AEROACÚSTICA, ENGENHARIA AERONÁUTICA

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      SPILLERE, André M. N. et al. Inlet liner design for a fan noise test rig. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-2724. Acesso em: 05 nov. 2024.
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      Spillere, A. M. N., Braga, D. S., Seki, L. A., Bonomo, L. A., Cordioli, J. A., Rocamora Junior, B. M., et al. (2019). Inlet liner design for a fan noise test rig. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-2724
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      Spillere AMN, Braga DS, Seki LA, Bonomo LA, Cordioli JA, Rocamora Junior BM, Greco Júnior PC, Reis DC dos, Coelho ELC. Inlet liner design for a fan noise test rig [Internet]. Proceedings. 2019 ;[citado 2024 nov. 05 ] Available from: https://doi.org/10.2514/6.2019-2724
    • Vancouver

      Spillere AMN, Braga DS, Seki LA, Bonomo LA, Cordioli JA, Rocamora Junior BM, Greco Júnior PC, Reis DC dos, Coelho ELC. Inlet liner design for a fan noise test rig [Internet]. Proceedings. 2019 ;[citado 2024 nov. 05 ] Available from: https://doi.org/10.2514/6.2019-2724
  • Source: Proceedings. Conference titles: AIAA Scitech Forum. Unidade: EESC

    Subjects: AEROFÓLIOS, AEROELASTICIDADE DE AERONAVES, ENGENHARIA MECÂNICA

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      SANTOS, Carlos Renan dos e MARQUES, Flavio Donizeti. Stall-induced oscillations of typical aeroelastic sections in low airspeeds. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-0610. Acesso em: 05 nov. 2024.
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      Santos, C. R. dos, & Marques, F. D. (2019). Stall-induced oscillations of typical aeroelastic sections in low airspeeds. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-0610
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      Santos CR dos, Marques FD. Stall-induced oscillations of typical aeroelastic sections in low airspeeds [Internet]. Proceedings. 2019 ;[citado 2024 nov. 05 ] Available from: https://doi.org/10.2514/6.2019-0610
    • Vancouver

      Santos CR dos, Marques FD. Stall-induced oscillations of typical aeroelastic sections in low airspeeds [Internet]. Proceedings. 2019 ;[citado 2024 nov. 05 ] Available from: https://doi.org/10.2514/6.2019-0610
  • Source: Proceedings. Conference titles: AIAA/CEAS Aeroacoustics Conference. Unidade: EESC

    Subjects: FLAPS, AEROACÚSTICA, AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA

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      ACEVEDO GIRALDO, Daniel et al. Experimental aeroacoustic and aerodynamic analysis of a large-scale flap side-edge model. 2018, Anais.. Reston, VA, USA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-3799. Acesso em: 05 nov. 2024.
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      Acevedo Giraldo, D., Botero Bolívar, L., Pereira, L. T. L., Catalano, F. M., Reis, D. C. dos, & Coelho, E. L. C. (2018). Experimental aeroacoustic and aerodynamic analysis of a large-scale flap side-edge model. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2018-3799
    • NLM

      Acevedo Giraldo D, Botero Bolívar L, Pereira LTL, Catalano FM, Reis DC dos, Coelho ELC. Experimental aeroacoustic and aerodynamic analysis of a large-scale flap side-edge model [Internet]. Proceedings. 2018 ;[citado 2024 nov. 05 ] Available from: https://doi.org/10.2514/6.2018-3799
    • Vancouver

      Acevedo Giraldo D, Botero Bolívar L, Pereira LTL, Catalano FM, Reis DC dos, Coelho ELC. Experimental aeroacoustic and aerodynamic analysis of a large-scale flap side-edge model [Internet]. Proceedings. 2018 ;[citado 2024 nov. 05 ] Available from: https://doi.org/10.2514/6.2018-3799
  • Source: Proceedings. Conference titles: AIAA/CEAS Aeroacoustics Conference. Unidade: EESC

    Subjects: AEROACÚSTICA, SLATS, ENGENHARIA AERONÁUTICA

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      BOTERO BOLÍVAR, Laura et al. Parametric analysis of the influence of slat geometry on acoustic noise. 2018, Anais.. Reston, VA, USA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-3593. Acesso em: 05 nov. 2024.
    • APA

      Botero Bolívar, L., Pereira, L. T. L., Acevedo Giraldo, D., Catalano, F. M., Reis, D. C. dos, & Coelho, E. L. C. (2018). Parametric analysis of the influence of slat geometry on acoustic noise. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2018-3593
    • NLM

      Botero Bolívar L, Pereira LTL, Acevedo Giraldo D, Catalano FM, Reis DC dos, Coelho ELC. Parametric analysis of the influence of slat geometry on acoustic noise [Internet]. Proceedings. 2018 ;[citado 2024 nov. 05 ] Available from: https://doi.org/10.2514/6.2018-3593
    • Vancouver

      Botero Bolívar L, Pereira LTL, Acevedo Giraldo D, Catalano FM, Reis DC dos, Coelho ELC. Parametric analysis of the influence of slat geometry on acoustic noise [Internet]. Proceedings. 2018 ;[citado 2024 nov. 05 ] Available from: https://doi.org/10.2514/6.2018-3593
  • Source: Proceedings. Conference titles: AAIA Aerospace Sciences Meeting. Unidade: EESC

    Subjects: TRENS DE POUSO, ENGENHARIA AERONÁUTICA, AERODINÂMICA DE AERONAVES, AEROACÚSTICA

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      REGO, Leandro Falcão Loureiro et al. Aerodynamic and aeroacoustic experimental investigation of a simplified nose landing gear. 2018, Anais.. Reston, VA, USA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-0759. Acesso em: 05 nov. 2024.
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      Rego, L. F. L., Pereira, L. T. L., Catalano, F. M., Speth, R., Bent, P., & Fregnani, J. A. (2018). Aerodynamic and aeroacoustic experimental investigation of a simplified nose landing gear. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2018-0759
    • NLM

      Rego LFL, Pereira LTL, Catalano FM, Speth R, Bent P, Fregnani JA. Aerodynamic and aeroacoustic experimental investigation of a simplified nose landing gear [Internet]. Proceedings. 2018 ;[citado 2024 nov. 05 ] Available from: https://doi.org/10.2514/6.2018-0759
    • Vancouver

      Rego LFL, Pereira LTL, Catalano FM, Speth R, Bent P, Fregnani JA. Aerodynamic and aeroacoustic experimental investigation of a simplified nose landing gear [Internet]. Proceedings. 2018 ;[citado 2024 nov. 05 ] Available from: https://doi.org/10.2514/6.2018-0759
  • Source: Proceedings. Conference titles: AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Unidade: EESC

    Subjects: AEROELASTICIDADE DE AERONAVES, AEROFÓLIOS, ENGENHARIA MECÂNICA

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      SANTOS, Carlos Renan dos e MARQUES, Flavio Donizeti e HAJJ, Muhammad R. Structural nonlinearities influence on the energy harvesting from stall-induced oscillations. 2018, Anais.. Reston, VA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-0464. Acesso em: 05 nov. 2024.
    • APA

      Santos, C. R. dos, Marques, F. D., & Hajj, M. R. (2018). Structural nonlinearities influence on the energy harvesting from stall-induced oscillations. In Proceedings. Reston, VA: AIAA. doi:10.2514/6.2018-0464
    • NLM

      Santos CR dos, Marques FD, Hajj MR. Structural nonlinearities influence on the energy harvesting from stall-induced oscillations [Internet]. Proceedings. 2018 ;[citado 2024 nov. 05 ] Available from: https://doi.org/10.2514/6.2018-0464
    • Vancouver

      Santos CR dos, Marques FD, Hajj MR. Structural nonlinearities influence on the energy harvesting from stall-induced oscillations [Internet]. Proceedings. 2018 ;[citado 2024 nov. 05 ] Available from: https://doi.org/10.2514/6.2018-0464

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