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ABNT
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: 18 nov. 2025.
APA
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 2025 nov. 18 ] 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 2025 nov. 18 ] Available from: https://doi.org/10.2514/6.2019-3695
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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: 18 nov. 2025.
APA
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
NLM
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 2025 nov. 18 ] 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 2025 nov. 18 ] Available from: https://doi.org/10.2514/6.2019-2700
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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: 18 nov. 2025.
APA
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
NLM
Mathias MS, Medeiros MAF de. Global instability analysis of a boundary layer flow over a small cavity [Internet]. Proceedings. 2019 ;[citado 2025 nov. 18 ] 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 2025 nov. 18 ] Available from: https://doi.org/10.2514/6.2019-3535
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MATHIAS, Marlon Sproesser e MEDEIROS, Marcello Augusto Faraco de. The influence of the boundary layer thickness on the stability of the Rossiter modes of a compressible rectangular cavity. 2018, Anais.. Reston, VA, USA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-3386. Acesso em: 18 nov. 2025.
APA
Mathias, M. S., & Medeiros, M. A. F. de. (2018). The influence of the boundary layer thickness on the stability of the Rossiter modes of a compressible rectangular cavity. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2018-3386
NLM
Mathias MS, Medeiros MAF de. The influence of the boundary layer thickness on the stability of the Rossiter modes of a compressible rectangular cavity [Internet]. Proceedings. 2018 ;[citado 2025 nov. 18 ] Available from: https://doi.org/10.2514/6.2018-3386
Vancouver
Mathias MS, Medeiros MAF de. The influence of the boundary layer thickness on the stability of the Rossiter modes of a compressible rectangular cavity [Internet]. Proceedings. 2018 ;[citado 2025 nov. 18 ] Available from: https://doi.org/10.2514/6.2018-3386
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SERRANO RICO, Juan Carlos et al. Low acoustic noise and turbulence (LANT) wind-tunnel at USP-EESC. 2018, Anais.. Reston, VA, USA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-3960. Acesso em: 18 nov. 2025.
APA
Serrano Rico, J. C., Amaral, F. R. do, Bresci, C. S., Beraldo, M. M., & Medeiros, M. A. F. de. (2018). Low acoustic noise and turbulence (LANT) wind-tunnel at USP-EESC. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2018-3960
NLM
Serrano Rico JC, Amaral FR do, Bresci CS, Beraldo MM, Medeiros MAF de. Low acoustic noise and turbulence (LANT) wind-tunnel at USP-EESC [Internet]. Proceedings. 2018 ;[citado 2025 nov. 18 ] Available from: https://doi.org/10.2514/6.2018-3960
Vancouver
Serrano Rico JC, Amaral FR do, Bresci CS, Beraldo MM, Medeiros MAF de. Low acoustic noise and turbulence (LANT) wind-tunnel at USP-EESC [Internet]. Proceedings. 2018 ;[citado 2025 nov. 18 ] Available from: https://doi.org/10.2514/6.2018-3960
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GAVIRIA MARTÍNEZ, Germán Andrés e MEDEIROS, Marcello Augusto Faraco de. Direct numerical simulation of a wavepacket in a boundary layer at Mach 0.9. 2016, Anais.. Reston, VA, USA: AIAA, 2016. Disponível em: https://repositorio.usp.br/directbitstream/df087384-f496-47c5-9df7-634fbd8ac6bb/trabalho%2018%20-%20Direct%20numerical%20simulation%20of%20a%20wavepacket%20in%20a%20boundary%20layer%20at%20Mach%200.9%20%2846th%20AIAA%20Fluid%20Dynamics%20Conference%2C%202016%29.pdf. Acesso em: 18 nov. 2025.
APA
Gaviria Martínez, G. A., & Medeiros, M. A. F. de. (2016). Direct numerical simulation of a wavepacket in a boundary layer at Mach 0.9. In Proceedings. Reston, VA, USA: AIAA. Recuperado de https://repositorio.usp.br/directbitstream/df087384-f496-47c5-9df7-634fbd8ac6bb/trabalho%2018%20-%20Direct%20numerical%20simulation%20of%20a%20wavepacket%20in%20a%20boundary%20layer%20at%20Mach%200.9%20%2846th%20AIAA%20Fluid%20Dynamics%20Conference%2C%202016%29.pdf
NLM
Gaviria Martínez GA, Medeiros MAF de. Direct numerical simulation of a wavepacket in a boundary layer at Mach 0.9 [Internet]. Proceedings. 2016 ;[citado 2025 nov. 18 ] Available from: https://repositorio.usp.br/directbitstream/df087384-f496-47c5-9df7-634fbd8ac6bb/trabalho%2018%20-%20Direct%20numerical%20simulation%20of%20a%20wavepacket%20in%20a%20boundary%20layer%20at%20Mach%200.9%20%2846th%20AIAA%20Fluid%20Dynamics%20Conference%2C%202016%29.pdf
Vancouver
Gaviria Martínez GA, Medeiros MAF de. Direct numerical simulation of a wavepacket in a boundary layer at Mach 0.9 [Internet]. Proceedings. 2016 ;[citado 2025 nov. 18 ] Available from: https://repositorio.usp.br/directbitstream/df087384-f496-47c5-9df7-634fbd8ac6bb/trabalho%2018%20-%20Direct%20numerical%20simulation%20of%20a%20wavepacket%20in%20a%20boundary%20layer%20at%20Mach%200.9%20%2846th%20AIAA%20Fluid%20Dynamics%20Conference%2C%202016%29.pdf
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AMARAL, Filipe Ramos do e PAGANI JÚNIOR, Carlos do Carmo e MEDEIROS, Marcello Augusto Faraco de. Experiments on slat noise from −6◦ to 18◦ angles of attack. 2016, Anais.. Reston, VA, USA: AIAA, 2016. Disponível em: https://repositorio.usp.br/directbitstream/22944961-1231-4c8b-83df-579d6d68e5df/trabalho%2019%20-%20Experiments%20on%20Slat%20Noise%20from%20-6%C2%B0%20to%2018%C2%B0%20Angles%20of%20Attack%20%2846th%20AIAA%20Fluid%20Dynamics%20Conference%2C%202016%29.pdf. Acesso em: 18 nov. 2025.
APA
Amaral, F. R. do, Pagani Júnior, C. do C., & Medeiros, M. A. F. de. (2016). Experiments on slat noise from −6◦ to 18◦ angles of attack. In Proceedings. Reston, VA, USA: AIAA. Recuperado de https://repositorio.usp.br/directbitstream/22944961-1231-4c8b-83df-579d6d68e5df/trabalho%2019%20-%20Experiments%20on%20Slat%20Noise%20from%20-6%C2%B0%20to%2018%C2%B0%20Angles%20of%20Attack%20%2846th%20AIAA%20Fluid%20Dynamics%20Conference%2C%202016%29.pdf
NLM
Amaral FR do, Pagani Júnior C do C, Medeiros MAF de. Experiments on slat noise from −6◦ to 18◦ angles of attack [Internet]. Proceedings. 2016 ;[citado 2025 nov. 18 ] Available from: https://repositorio.usp.br/directbitstream/22944961-1231-4c8b-83df-579d6d68e5df/trabalho%2019%20-%20Experiments%20on%20Slat%20Noise%20from%20-6%C2%B0%20to%2018%C2%B0%20Angles%20of%20Attack%20%2846th%20AIAA%20Fluid%20Dynamics%20Conference%2C%202016%29.pdf
Vancouver
Amaral FR do, Pagani Júnior C do C, Medeiros MAF de. Experiments on slat noise from −6◦ to 18◦ angles of attack [Internet]. Proceedings. 2016 ;[citado 2025 nov. 18 ] Available from: https://repositorio.usp.br/directbitstream/22944961-1231-4c8b-83df-579d6d68e5df/trabalho%2019%20-%20Experiments%20on%20Slat%20Noise%20from%20-6%C2%B0%20to%2018%C2%B0%20Angles%20of%20Attack%20%2846th%20AIAA%20Fluid%20Dynamics%20Conference%2C%202016%29.pdf
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AMARAL, Filipe Ramos do et al. Experimental study of the effect of a small 2D excrescence placed on the slat cove surface of an airfoil on its acoustic noise. 2015, Anais.. Reston, VA, USA: AIAA, 2015. Disponível em: https://repositorio.usp.br/directbitstream/ac1cb72d-ea75-49d8-bba4-27e0e561cf61/trabalho%2022%20-%20Experimental%20study%20of%20the%20effect%20of%20a%20small%202D%20excrescence%20placed%20on%20the%20slat%20cove%20surface%20of%20an%20airfoil%20on%20its%20acoustic%20noise%20%2821st%20AIAACEAS%20Aeroacoustics%20Conference%202015%29.pdf. Acesso em: 18 nov. 2025.
APA
Amaral, F. R. do, Souza, D. S., Pagani Júnior, C. do C., Himeno, F. H. T., & Medeiros, M. A. F. de. (2015). Experimental study of the effect of a small 2D excrescence placed on the slat cove surface of an airfoil on its acoustic noise. In Proceedings. Reston, VA, USA: AIAA. Recuperado de https://repositorio.usp.br/directbitstream/ac1cb72d-ea75-49d8-bba4-27e0e561cf61/trabalho%2022%20-%20Experimental%20study%20of%20the%20effect%20of%20a%20small%202D%20excrescence%20placed%20on%20the%20slat%20cove%20surface%20of%20an%20airfoil%20on%20its%20acoustic%20noise%20%2821st%20AIAACEAS%20Aeroacoustics%20Conference%202015%29.pdf
NLM
Amaral FR do, Souza DS, Pagani Júnior C do C, Himeno FHT, Medeiros MAF de. Experimental study of the effect of a small 2D excrescence placed on the slat cove surface of an airfoil on its acoustic noise [Internet]. Proceedings. 2015 ;[citado 2025 nov. 18 ] Available from: https://repositorio.usp.br/directbitstream/ac1cb72d-ea75-49d8-bba4-27e0e561cf61/trabalho%2022%20-%20Experimental%20study%20of%20the%20effect%20of%20a%20small%202D%20excrescence%20placed%20on%20the%20slat%20cove%20surface%20of%20an%20airfoil%20on%20its%20acoustic%20noise%20%2821st%20AIAACEAS%20Aeroacoustics%20Conference%202015%29.pdf
Vancouver
Amaral FR do, Souza DS, Pagani Júnior C do C, Himeno FHT, Medeiros MAF de. Experimental study of the effect of a small 2D excrescence placed on the slat cove surface of an airfoil on its acoustic noise [Internet]. Proceedings. 2015 ;[citado 2025 nov. 18 ] Available from: https://repositorio.usp.br/directbitstream/ac1cb72d-ea75-49d8-bba4-27e0e561cf61/trabalho%2022%20-%20Experimental%20study%20of%20the%20effect%20of%20a%20small%202D%20excrescence%20placed%20on%20the%20slat%20cove%20surface%20of%20an%20airfoil%20on%20its%20acoustic%20noise%20%2821st%20AIAACEAS%20Aeroacoustics%20Conference%202015%29.pdf
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SOUZA, Daniel Sampaio e RODRIGUEZ, Daniel e MEDEIROS, Marcello Augusto Faraco de. A study of the sources of slat noise using proper orthogonal decomposition. 2013, Anais.. Reston, VA, USA: AIAA, 2013. Disponível em: https://repositorio.usp.br/directbitstream/fdc144b2-1c1d-4ea3-a1d8-84f66f3a61a1/trabalho%2031%20-%20A%20Study%20of%20the%20Sources%20of%20Slat%20Noise%20using%20Proper%20Orthogonal%20Decomposition%20%2819th%20AIAA-CEAS%20Aeroacoustics%20Conference%2C%202013%2C%20Berlin%29.pdf. Acesso em: 18 nov. 2025.
APA
Souza, D. S., Rodriguez, D., & Medeiros, M. A. F. de. (2013). A study of the sources of slat noise using proper orthogonal decomposition. In Proceedings. Reston, VA, USA: AIAA. Recuperado de https://repositorio.usp.br/directbitstream/fdc144b2-1c1d-4ea3-a1d8-84f66f3a61a1/trabalho%2031%20-%20A%20Study%20of%20the%20Sources%20of%20Slat%20Noise%20using%20Proper%20Orthogonal%20Decomposition%20%2819th%20AIAA-CEAS%20Aeroacoustics%20Conference%2C%202013%2C%20Berlin%29.pdf
NLM
Souza DS, Rodriguez D, Medeiros MAF de. A study of the sources of slat noise using proper orthogonal decomposition [Internet]. Proceedings. 2013 ;[citado 2025 nov. 18 ] Available from: https://repositorio.usp.br/directbitstream/fdc144b2-1c1d-4ea3-a1d8-84f66f3a61a1/trabalho%2031%20-%20A%20Study%20of%20the%20Sources%20of%20Slat%20Noise%20using%20Proper%20Orthogonal%20Decomposition%20%2819th%20AIAA-CEAS%20Aeroacoustics%20Conference%2C%202013%2C%20Berlin%29.pdf
Vancouver
Souza DS, Rodriguez D, Medeiros MAF de. A study of the sources of slat noise using proper orthogonal decomposition [Internet]. Proceedings. 2013 ;[citado 2025 nov. 18 ] Available from: https://repositorio.usp.br/directbitstream/fdc144b2-1c1d-4ea3-a1d8-84f66f3a61a1/trabalho%2031%20-%20A%20Study%20of%20the%20Sources%20of%20Slat%20Noise%20using%20Proper%20Orthogonal%20Decomposition%20%2819th%20AIAA-CEAS%20Aeroacoustics%20Conference%2C%202013%2C%20Berlin%29.pdf
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BERGAMO, Leandro Fernandes e GENNARO, Elmer Mateus e MEDEIROS, Marcello Augusto Faraco de. Effect of Mach number on linear stability of lid-driven cavity flows. 2013, Anais.. Reston, VA, USA: AIAA, 2013. Disponível em: https://repositorio.usp.br/directbitstream/3c08812e-2db5-4341-a673-36520c033fa4/trabalho%2032%20-%20Effect%20of%20Mach%20number%20on%20linear%20stability%20of%20lid-driven%20cavity%20flows%20%2843%20AIAA%20Fluid%20Dynamics%20Conference%202013%29.pdf. Acesso em: 18 nov. 2025.
APA
Bergamo, L. F., Gennaro, E. M., & Medeiros, M. A. F. de. (2013). Effect of Mach number on linear stability of lid-driven cavity flows. In Proceedings. Reston, VA, USA: AIAA. Recuperado de https://repositorio.usp.br/directbitstream/3c08812e-2db5-4341-a673-36520c033fa4/trabalho%2032%20-%20Effect%20of%20Mach%20number%20on%20linear%20stability%20of%20lid-driven%20cavity%20flows%20%2843%20AIAA%20Fluid%20Dynamics%20Conference%202013%29.pdf
NLM
Bergamo LF, Gennaro EM, Medeiros MAF de. Effect of Mach number on linear stability of lid-driven cavity flows [Internet]. Proceedings. 2013 ;[citado 2025 nov. 18 ] Available from: https://repositorio.usp.br/directbitstream/3c08812e-2db5-4341-a673-36520c033fa4/trabalho%2032%20-%20Effect%20of%20Mach%20number%20on%20linear%20stability%20of%20lid-driven%20cavity%20flows%20%2843%20AIAA%20Fluid%20Dynamics%20Conference%202013%29.pdf
Vancouver
Bergamo LF, Gennaro EM, Medeiros MAF de. Effect of Mach number on linear stability of lid-driven cavity flows [Internet]. Proceedings. 2013 ;[citado 2025 nov. 18 ] Available from: https://repositorio.usp.br/directbitstream/3c08812e-2db5-4341-a673-36520c033fa4/trabalho%2032%20-%20Effect%20of%20Mach%20number%20on%20linear%20stability%20of%20lid-driven%20cavity%20flows%20%2843%20AIAA%20Fluid%20Dynamics%20Conference%202013%29.pdf
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BANDLE, Lukas et al. On detrimental effects of excrescences on the slat noise. 2012, Anais.. Reston, VA, USA: AIAA, 2012. Disponível em: https://repositorio.usp.br/directbitstream/1cb1bc47-98f4-48c3-925c-45032f43fb0a/trabalho%2035%20-%20%20On%20Detrimental%20Effects%20of%20Excrescences%20on%20the%20Slat%20Noise%20%2818th%20AIAA-CEAS%20Aeroacoustics%20Conference%20%2833rd%20AIAA%20Aeroacoustics%20Conference%29%2C%202012%29.pdf. Acesso em: 18 nov. 2025.
APA
Bandle, L., Souza, D. S., Simões, L. G. C., & Medeiros, M. A. F. de. (2012). On detrimental effects of excrescences on the slat noise. In Proceedings. Reston, VA, USA: AIAA. Recuperado de https://repositorio.usp.br/directbitstream/1cb1bc47-98f4-48c3-925c-45032f43fb0a/trabalho%2035%20-%20%20On%20Detrimental%20Effects%20of%20Excrescences%20on%20the%20Slat%20Noise%20%2818th%20AIAA-CEAS%20Aeroacoustics%20Conference%20%2833rd%20AIAA%20Aeroacoustics%20Conference%29%2C%202012%29.pdf
NLM
Bandle L, Souza DS, Simões LGC, Medeiros MAF de. On detrimental effects of excrescences on the slat noise [Internet]. Proceedings. 2012 ;[citado 2025 nov. 18 ] Available from: https://repositorio.usp.br/directbitstream/1cb1bc47-98f4-48c3-925c-45032f43fb0a/trabalho%2035%20-%20%20On%20Detrimental%20Effects%20of%20Excrescences%20on%20the%20Slat%20Noise%20%2818th%20AIAA-CEAS%20Aeroacoustics%20Conference%20%2833rd%20AIAA%20Aeroacoustics%20Conference%29%2C%202012%29.pdf
Vancouver
Bandle L, Souza DS, Simões LGC, Medeiros MAF de. On detrimental effects of excrescences on the slat noise [Internet]. Proceedings. 2012 ;[citado 2025 nov. 18 ] Available from: https://repositorio.usp.br/directbitstream/1cb1bc47-98f4-48c3-925c-45032f43fb0a/trabalho%2035%20-%20%20On%20Detrimental%20Effects%20of%20Excrescences%20on%20the%20Slat%20Noise%20%2818th%20AIAA-CEAS%20Aeroacoustics%20Conference%20%2833rd%20AIAA%20Aeroacoustics%20Conference%29%2C%202012%29.pdf
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MOSER, Carlos A. S. e MEDEIROS, Marcello Augusto Faraco de. Non-conservative implicit large-eddy simulation method for predicting the noise radiated by subsonic jets. 2012, Anais.. Reston, VA, USA: AIAA, 2012. Disponível em: https://repositorio.usp.br/directbitstream/7cce9af7-1148-4451-b977-b5bf72d29345/trabalho%2034%20-%20Non-conservative%20implicit%20large-eddy%20simulation%20method%20for%20predicting%20the%20noise%20radiated%20by%20subsonic%20jets%20%2818th%20AIAA-CEAS%20Aeroacoustics%20Conference%29_removed.pdf. Acesso em: 18 nov. 2025.
APA
Moser, C. A. S., & Medeiros, M. A. F. de. (2012). Non-conservative implicit large-eddy simulation method for predicting the noise radiated by subsonic jets. In Proceedings. Reston, VA, USA: AIAA. Recuperado de https://repositorio.usp.br/directbitstream/7cce9af7-1148-4451-b977-b5bf72d29345/trabalho%2034%20-%20Non-conservative%20implicit%20large-eddy%20simulation%20method%20for%20predicting%20the%20noise%20radiated%20by%20subsonic%20jets%20%2818th%20AIAA-CEAS%20Aeroacoustics%20Conference%29_removed.pdf
NLM
Moser CAS, Medeiros MAF de. Non-conservative implicit large-eddy simulation method for predicting the noise radiated by subsonic jets [Internet]. Proceedings. 2012 ;[citado 2025 nov. 18 ] Available from: https://repositorio.usp.br/directbitstream/7cce9af7-1148-4451-b977-b5bf72d29345/trabalho%2034%20-%20Non-conservative%20implicit%20large-eddy%20simulation%20method%20for%20predicting%20the%20noise%20radiated%20by%20subsonic%20jets%20%2818th%20AIAA-CEAS%20Aeroacoustics%20Conference%29_removed.pdf
Vancouver
Moser CAS, Medeiros MAF de. Non-conservative implicit large-eddy simulation method for predicting the noise radiated by subsonic jets [Internet]. Proceedings. 2012 ;[citado 2025 nov. 18 ] Available from: https://repositorio.usp.br/directbitstream/7cce9af7-1148-4451-b977-b5bf72d29345/trabalho%2034%20-%20Non-conservative%20implicit%20large-eddy%20simulation%20method%20for%20predicting%20the%20noise%20radiated%20by%20subsonic%20jets%20%2818th%20AIAA-CEAS%20Aeroacoustics%20Conference%29_removed.pdf
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COUTINHO, Eduardo de Castro e MEDEIROS, Marcello Augusto Faraco de. High-order and high-accurate immersed interface method for uid dynamics. 2012, Anais.. São Paulo, SP: Escola de Engenharia de São Carlos, Universidade de São Paulo, 2012. Disponível em: https://repositorio.usp.br/directbitstream/85387cd4-3470-4900-939f-59160469e055/trabalho%2040%20-%20HIGH-ORDER%20AND%20HIGH-ACCURATE%20IMMERSED%20INTERFACE%20METHOD%20FOR%20FLUID%20DYNAMICS%20%2810th%20World%20Conference%20on%20Computational%20Mechanics%2C%202012%29.pdf. Acesso em: 18 nov. 2025.
APA
Coutinho, E. de C., & Medeiros, M. A. F. de. (2012). High-order and high-accurate immersed interface method for uid dynamics. In Proceedings. São Paulo, SP: Escola de Engenharia de São Carlos, Universidade de São Paulo. Recuperado de https://repositorio.usp.br/directbitstream/85387cd4-3470-4900-939f-59160469e055/trabalho%2040%20-%20HIGH-ORDER%20AND%20HIGH-ACCURATE%20IMMERSED%20INTERFACE%20METHOD%20FOR%20FLUID%20DYNAMICS%20%2810th%20World%20Conference%20on%20Computational%20Mechanics%2C%202012%29.pdf
NLM
Coutinho E de C, Medeiros MAF de. High-order and high-accurate immersed interface method for uid dynamics [Internet]. Proceedings. 2012 ;[citado 2025 nov. 18 ] Available from: https://repositorio.usp.br/directbitstream/85387cd4-3470-4900-939f-59160469e055/trabalho%2040%20-%20HIGH-ORDER%20AND%20HIGH-ACCURATE%20IMMERSED%20INTERFACE%20METHOD%20FOR%20FLUID%20DYNAMICS%20%2810th%20World%20Conference%20on%20Computational%20Mechanics%2C%202012%29.pdf
Vancouver
Coutinho E de C, Medeiros MAF de. High-order and high-accurate immersed interface method for uid dynamics [Internet]. Proceedings. 2012 ;[citado 2025 nov. 18 ] Available from: https://repositorio.usp.br/directbitstream/85387cd4-3470-4900-939f-59160469e055/trabalho%2040%20-%20HIGH-ORDER%20AND%20HIGH-ACCURATE%20IMMERSED%20INTERFACE%20METHOD%20FOR%20FLUID%20DYNAMICS%20%2810th%20World%20Conference%20on%20Computational%20Mechanics%2C%202012%29.pdf
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ABNT
GENNARO, Elmer Mateus e BERGAMO, Leandro Fernandes e MEDEIROS, Marcello Augusto Faraco de. Wavepackets in a compressible subsonic adverse pressure gradient boundary layer. 2012, Anais.. Reston, VA, USA: AIAA, 2012. . Acesso em: 18 nov. 2025.
APA
Gennaro, E. M., Bergamo, L. F., & Medeiros, M. A. F. de. (2012). Wavepackets in a compressible subsonic adverse pressure gradient boundary layer. In Proceedings. Reston, VA, USA: AIAA.
NLM
Gennaro EM, Bergamo LF, Medeiros MAF de. Wavepackets in a compressible subsonic adverse pressure gradient boundary layer. Proceedings. 2012 ;[citado 2025 nov. 18 ]
Vancouver
Gennaro EM, Bergamo LF, Medeiros MAF de. Wavepackets in a compressible subsonic adverse pressure gradient boundary layer. Proceedings. 2012 ;[citado 2025 nov. 18 ]
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ABNT
SIMÕES, Leandro Guilherme Crenite e SOUZA, Daniel Sampaio e MEDEIROS, Marcello Augusto Faraco de. On the small effect of boundary layer thicknesses on slat noise. 2011, Anais.. Reston, VA, USA: AIAA, 2011. Disponível em: https://repositorio.usp.br/directbitstream/183d35df-df3b-4268-8d8b-65e4ba9e660d/trabalho%2043%20-%20On%20the%20Small%20Effect%20of%20Boundary%20Layer%20Thicknesses%20on%20Slat%20Noise%20%2817th%20AIAA-CEAS%20Aeroacoustics%20Conference%20%2832nd%20AIAA%20Aeroacoustics%20Conference%29%2C%202011%29.pdf. Acesso em: 18 nov. 2025.
APA
Simões, L. G. C., Souza, D. S., & Medeiros, M. A. F. de. (2011). On the small effect of boundary layer thicknesses on slat noise. In Proceedings. Reston, VA, USA: AIAA. Recuperado de https://repositorio.usp.br/directbitstream/183d35df-df3b-4268-8d8b-65e4ba9e660d/trabalho%2043%20-%20On%20the%20Small%20Effect%20of%20Boundary%20Layer%20Thicknesses%20on%20Slat%20Noise%20%2817th%20AIAA-CEAS%20Aeroacoustics%20Conference%20%2832nd%20AIAA%20Aeroacoustics%20Conference%29%2C%202011%29.pdf
NLM
Simões LGC, Souza DS, Medeiros MAF de. On the small effect of boundary layer thicknesses on slat noise [Internet]. Proceedings. 2011 ;[citado 2025 nov. 18 ] Available from: https://repositorio.usp.br/directbitstream/183d35df-df3b-4268-8d8b-65e4ba9e660d/trabalho%2043%20-%20On%20the%20Small%20Effect%20of%20Boundary%20Layer%20Thicknesses%20on%20Slat%20Noise%20%2817th%20AIAA-CEAS%20Aeroacoustics%20Conference%20%2832nd%20AIAA%20Aeroacoustics%20Conference%29%2C%202011%29.pdf
Vancouver
Simões LGC, Souza DS, Medeiros MAF de. On the small effect of boundary layer thicknesses on slat noise [Internet]. Proceedings. 2011 ;[citado 2025 nov. 18 ] Available from: https://repositorio.usp.br/directbitstream/183d35df-df3b-4268-8d8b-65e4ba9e660d/trabalho%2043%20-%20On%20the%20Small%20Effect%20of%20Boundary%20Layer%20Thicknesses%20on%20Slat%20Noise%20%2817th%20AIAA-CEAS%20Aeroacoustics%20Conference%20%2832nd%20AIAA%20Aeroacoustics%20Conference%29%2C%202011%29.pdf
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SANTANA, Leandro Dantas et al. The update process and characterization of the Sao Paulo University wind-tunnel for aeroacoustics testing. 2010, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2010. . Acesso em: 18 nov. 2025.
APA
Santana, L. D., Catalano, F. M., Medeiros, M. A. F. de, & Carmo, M. (2010). The update process and characterization of the Sao Paulo University wind-tunnel for aeroacoustics testing. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS.
NLM
Santana LD, Catalano FM, Medeiros MAF de, Carmo M. The update process and characterization of the Sao Paulo University wind-tunnel for aeroacoustics testing. Proceedings. 2010 ;[citado 2025 nov. 18 ]
Vancouver
Santana LD, Catalano FM, Medeiros MAF de, Carmo M. The update process and characterization of the Sao Paulo University wind-tunnel for aeroacoustics testing. Proceedings. 2010 ;[citado 2025 nov. 18 ]
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ABNT
SILVA, Homero Ghioti da e MEDEIROS, Marcello Augusto Faraco de e MOSER, Carlos Anissem Soares. Influence of boundary conditions on the order of accuracy of a mixed high-order numerical code. 2010, Anais.. Lisboa, Portugal: APMTAC/IDMEC, 2010. Disponível em: https://repositorio.usp.br/directbitstream/c5834110-9eee-4412-a295-adb7c10ec667/trabalho%2052%20-%20Influence%20of%20Boundary%20Conditions%20on%20the%20Order%20of%20Accuracy%20of%20a%20Mixed%20High-Order%20Numerical%20Code%20%28ECCOMAS%20CFD%202010%29.pdf. Acesso em: 18 nov. 2025.
APA
Silva, H. G. da, Medeiros, M. A. F. de, & Moser, C. A. S. (2010). Influence of boundary conditions on the order of accuracy of a mixed high-order numerical code. In Proceedings. Lisboa, Portugal: APMTAC/IDMEC. Recuperado de https://repositorio.usp.br/directbitstream/c5834110-9eee-4412-a295-adb7c10ec667/trabalho%2052%20-%20Influence%20of%20Boundary%20Conditions%20on%20the%20Order%20of%20Accuracy%20of%20a%20Mixed%20High-Order%20Numerical%20Code%20%28ECCOMAS%20CFD%202010%29.pdf
NLM
Silva HG da, Medeiros MAF de, Moser CAS. Influence of boundary conditions on the order of accuracy of a mixed high-order numerical code [Internet]. Proceedings. 2010 ;[citado 2025 nov. 18 ] Available from: https://repositorio.usp.br/directbitstream/c5834110-9eee-4412-a295-adb7c10ec667/trabalho%2052%20-%20Influence%20of%20Boundary%20Conditions%20on%20the%20Order%20of%20Accuracy%20of%20a%20Mixed%20High-Order%20Numerical%20Code%20%28ECCOMAS%20CFD%202010%29.pdf
Vancouver
Silva HG da, Medeiros MAF de, Moser CAS. Influence of boundary conditions on the order of accuracy of a mixed high-order numerical code [Internet]. Proceedings. 2010 ;[citado 2025 nov. 18 ] Available from: https://repositorio.usp.br/directbitstream/c5834110-9eee-4412-a295-adb7c10ec667/trabalho%2052%20-%20Influence%20of%20Boundary%20Conditions%20on%20the%20Order%20of%20Accuracy%20of%20a%20Mixed%20High-Order%20Numerical%20Code%20%28ECCOMAS%20CFD%202010%29.pdf
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MOSER, Carlos Anissem Soares e SILVESTRINI, Jorge Hugo e MEDEIROS, Marcello Augusto Faraco de. Implicit large-eddy simulation of noise radiated by a subsonic jet at high Reynolds number. 2010, Anais.. Lisboa, Portugal: APMTAC/IDMEC, 2010. Disponível em: https://repositorio.usp.br/directbitstream/4fbb8faf-4b52-4112-9efb-6a1566e1f9f7/trabalho%2050%20-%20Implicit%20large-eddy%20simulation%20of%20noise%20radiated%20by%20a%20Mach%200.90%20jet%20at%20high%20Reynolds%20number%20%28V%20European%20Conference%20on%20Computational%20Fluid%20Dynamics%2C%202010%29%20%281%29.pdf. Acesso em: 18 nov. 2025.
APA
Moser, C. A. S., Silvestrini, J. H., & Medeiros, M. A. F. de. (2010). Implicit large-eddy simulation of noise radiated by a subsonic jet at high Reynolds number. In Proceedings. Lisboa, Portugal: APMTAC/IDMEC. Recuperado de https://repositorio.usp.br/directbitstream/4fbb8faf-4b52-4112-9efb-6a1566e1f9f7/trabalho%2050%20-%20Implicit%20large-eddy%20simulation%20of%20noise%20radiated%20by%20a%20Mach%200.90%20jet%20at%20high%20Reynolds%20number%20%28V%20European%20Conference%20on%20Computational%20Fluid%20Dynamics%2C%202010%29%20%281%29.pdf
NLM
Moser CAS, Silvestrini JH, Medeiros MAF de. Implicit large-eddy simulation of noise radiated by a subsonic jet at high Reynolds number [Internet]. Proceedings. 2010 ;[citado 2025 nov. 18 ] Available from: https://repositorio.usp.br/directbitstream/4fbb8faf-4b52-4112-9efb-6a1566e1f9f7/trabalho%2050%20-%20Implicit%20large-eddy%20simulation%20of%20noise%20radiated%20by%20a%20Mach%200.90%20jet%20at%20high%20Reynolds%20number%20%28V%20European%20Conference%20on%20Computational%20Fluid%20Dynamics%2C%202010%29%20%281%29.pdf
Vancouver
Moser CAS, Silvestrini JH, Medeiros MAF de. Implicit large-eddy simulation of noise radiated by a subsonic jet at high Reynolds number [Internet]. Proceedings. 2010 ;[citado 2025 nov. 18 ] Available from: https://repositorio.usp.br/directbitstream/4fbb8faf-4b52-4112-9efb-6a1566e1f9f7/trabalho%2050%20-%20Implicit%20large-eddy%20simulation%20of%20noise%20radiated%20by%20a%20Mach%200.90%20jet%20at%20high%20Reynolds%20number%20%28V%20European%20Conference%20on%20Computational%20Fluid%20Dynamics%2C%202010%29%20%281%29.pdf
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BERGAMO, Leandro Fernandes e GENNARO, Elmer Mateus e MEDEIROS, Marcello Augusto Faraco de. Computational simulation of noise generated aerodynamically via DNS and acoustic analogy. 2010, Anais.. Edinburgh, UK: ICAS, 2010. Disponível em: https://repositorio.usp.br/directbitstream/ac40dddd-2a99-4358-99d0-11f3ac6cfa7c/trabalho%2053%20-%20Computational%20simulation%20of%20noise%20generated%20aerodynamically%20via%20DNS%20and%20acoustic%20analogy%20%28ICAS%202010%29_removed.pdf. Acesso em: 18 nov. 2025.
APA
Bergamo, L. F., Gennaro, E. M., & Medeiros, M. A. F. de. (2010). Computational simulation of noise generated aerodynamically via DNS and acoustic analogy. In Proceedings. Edinburgh, UK: ICAS. Recuperado de https://repositorio.usp.br/directbitstream/ac40dddd-2a99-4358-99d0-11f3ac6cfa7c/trabalho%2053%20-%20Computational%20simulation%20of%20noise%20generated%20aerodynamically%20via%20DNS%20and%20acoustic%20analogy%20%28ICAS%202010%29_removed.pdf
NLM
Bergamo LF, Gennaro EM, Medeiros MAF de. Computational simulation of noise generated aerodynamically via DNS and acoustic analogy [Internet]. Proceedings. 2010 ;[citado 2025 nov. 18 ] Available from: https://repositorio.usp.br/directbitstream/ac40dddd-2a99-4358-99d0-11f3ac6cfa7c/trabalho%2053%20-%20Computational%20simulation%20of%20noise%20generated%20aerodynamically%20via%20DNS%20and%20acoustic%20analogy%20%28ICAS%202010%29_removed.pdf
Vancouver
Bergamo LF, Gennaro EM, Medeiros MAF de. Computational simulation of noise generated aerodynamically via DNS and acoustic analogy [Internet]. Proceedings. 2010 ;[citado 2025 nov. 18 ] Available from: https://repositorio.usp.br/directbitstream/ac40dddd-2a99-4358-99d0-11f3ac6cfa7c/trabalho%2053%20-%20Computational%20simulation%20of%20noise%20generated%20aerodynamically%20via%20DNS%20and%20acoustic%20analogy%20%28ICAS%202010%29_removed.pdf
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ABNT
AFLALO, Bernardo S et al. Comparative analysis of turbulence models for slat noise source calculations employing unstructured meshes. 2010, Anais.. Reston, VA, USA: AIAA, 2010. Disponível em: https://repositorio.usp.br/directbitstream/89bd742a-6526-4bc0-86d6-624d174c8253/trabalho%2049%20-%20Comparative%20Analysis%20of%20Turbulence%20Models%20for%20Slat%20Noise%20Source%20Calculations%20Employing%20Unstructured%20Meshes%20%2816th%20AIAA-CEAS%20Aeroacoustics%20Conference%202010%29.pdf. Acesso em: 18 nov. 2025.
APA
Aflalo, B. S., Simões, L. G. C., Silva, R. G. da, & Medeiros, M. A. F. de. (2010). Comparative analysis of turbulence models for slat noise source calculations employing unstructured meshes. In Proceedings. Reston, VA, USA: AIAA. Recuperado de https://repositorio.usp.br/directbitstream/89bd742a-6526-4bc0-86d6-624d174c8253/trabalho%2049%20-%20Comparative%20Analysis%20of%20Turbulence%20Models%20for%20Slat%20Noise%20Source%20Calculations%20Employing%20Unstructured%20Meshes%20%2816th%20AIAA-CEAS%20Aeroacoustics%20Conference%202010%29.pdf
NLM
Aflalo BS, Simões LGC, Silva RG da, Medeiros MAF de. Comparative analysis of turbulence models for slat noise source calculations employing unstructured meshes [Internet]. Proceedings. 2010 ;[citado 2025 nov. 18 ] Available from: https://repositorio.usp.br/directbitstream/89bd742a-6526-4bc0-86d6-624d174c8253/trabalho%2049%20-%20Comparative%20Analysis%20of%20Turbulence%20Models%20for%20Slat%20Noise%20Source%20Calculations%20Employing%20Unstructured%20Meshes%20%2816th%20AIAA-CEAS%20Aeroacoustics%20Conference%202010%29.pdf
Vancouver
Aflalo BS, Simões LGC, Silva RG da, Medeiros MAF de. Comparative analysis of turbulence models for slat noise source calculations employing unstructured meshes [Internet]. Proceedings. 2010 ;[citado 2025 nov. 18 ] Available from: https://repositorio.usp.br/directbitstream/89bd742a-6526-4bc0-86d6-624d174c8253/trabalho%2049%20-%20Comparative%20Analysis%20of%20Turbulence%20Models%20for%20Slat%20Noise%20Source%20Calculations%20Employing%20Unstructured%20Meshes%20%2816th%20AIAA-CEAS%20Aeroacoustics%20Conference%202010%29.pdf
