A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
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: 27 maio 2024.
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 2024 maio 27 ] 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 maio 27 ] Available from: https://doi.org/10.2514/6.2019-2700
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
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: 27 maio 2024.
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 2024 maio 27 ] 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 maio 27 ] Available from: https://doi.org/10.2514/6.2019-3535
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
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: 27 maio 2024.
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 2024 maio 27 ] 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 2024 maio 27 ] Available from: https://doi.org/10.2514/6.2018-3386
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
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: 27 maio 2024.
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 2024 maio 27 ] 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 2024 maio 27 ] 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
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
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: 27 maio 2024.
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 2024 maio 27 ] 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 2024 maio 27 ] 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
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
AMARAL, Filipe Ramos do et al. Study of the effect of protusions on the slat noise using beamforming techniques and lattice-boltzmann method. 2014, Anais.. Ouro Preto, MG: ABMEC, 2014. . Acesso em: 27 maio 2024.
APA
Amaral, F. R. do, Himeno, F. H. T., Souza, D. S., Pagani Júnior, C. do C., Serrano Rico, J. C., & Medeiros, M. A. F. de. (2014). Study of the effect of protusions on the slat noise using beamforming techniques and lattice-boltzmann method. In Proceedings. Ouro Preto, MG: ABMEC.
NLM
Amaral FR do, Himeno FHT, Souza DS, Pagani Júnior C do C, Serrano Rico JC, Medeiros MAF de. Study of the effect of protusions on the slat noise using beamforming techniques and lattice-boltzmann method. Proceedings. 2014 ;[citado 2024 maio 27 ]
Vancouver
Amaral FR do, Himeno FHT, Souza DS, Pagani Júnior C do C, Serrano Rico JC, Medeiros MAF de. Study of the effect of protusions on the slat noise using beamforming techniques and lattice-boltzmann method. Proceedings. 2014 ;[citado 2024 maio 27 ]
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
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: 27 maio 2024.
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 2024 maio 27 ] 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 2024 maio 27 ] 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
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
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: 27 maio 2024.
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 2024 maio 27 ] 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 2024 maio 27 ] 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
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
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: 27 maio 2024.
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 2024 maio 27 ] 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 2024 maio 27 ] 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
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
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: 27 maio 2024.
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 2024 maio 27 ] 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 2024 maio 27 ] 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
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
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: 27 maio 2024.
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 2024 maio 27 ] 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 2024 maio 27 ] 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
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 27 maio 2024.
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 2024 maio 27 ]
Vancouver
Gennaro EM, Bergamo LF, Medeiros MAF de. Wavepackets in a compressible subsonic adverse pressure gradient boundary layer. Proceedings. 2012 ;[citado 2024 maio 27 ]
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 27 maio 2024.
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 2024 maio 27 ] 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 2024 maio 27 ] 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
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
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: 27 maio 2024.
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 2024 maio 27 ]
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 2024 maio 27 ]
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 27 maio 2024.
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 2024 maio 27 ] 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 2024 maio 27 ] 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
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
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: 27 maio 2024.
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 2024 maio 27 ] 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 2024 maio 27 ] 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
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
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: 27 maio 2024.
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 2024 maio 27 ] 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 2024 maio 27 ] 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
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 27 maio 2024.
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 2024 maio 27 ] 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 2024 maio 27 ] 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
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
ENTZ, Ricardo Maiko Uehoka et al. Methods for preliminary airfoil optimization. 2009, Anais.. Reston, VA, USA: AIAA, 2009. . Acesso em: 27 maio 2024.
APA
Entz, R. M. U., Correa, L. G. N., Oliveira, R. F. de, Catalano, F. M., & Medeiros, M. A. F. de. (2009). Methods for preliminary airfoil optimization. In Proceedings. Reston, VA, USA: AIAA.
NLM
Entz RMU, Correa LGN, Oliveira RF de, Catalano FM, Medeiros MAF de. Methods for preliminary airfoil optimization. Proceedings. 2009 ;[citado 2024 maio 27 ]
Vancouver
Entz RMU, Correa LGN, Oliveira RF de, Catalano FM, Medeiros MAF de. Methods for preliminary airfoil optimization. Proceedings. 2009 ;[citado 2024 maio 27 ]
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
MOSER, Carlos Anissem Soares e SILVESTRINI, Jorge Hugo e MEDEIROS, Marcello Augusto Faraco de. Investigation of the aerodynamic noise radiation by subsonic jets at high Reynolds. 2009, Anais.. London, UK: Royal Aeronautical Society, 2009. Disponível em: https://repositorio.usp.br/directbitstream/d7f212bd-ec7e-4ceb-b423-b58cf4285ed4/trabalho%2062%20-%20%20Investigation%20of%20the%20aerodynamic%20noise%20radiation%20by%20subsonic%20jets%20at%20high%20Reynolds%20%28European%20air%20and%20space%20conference%2C%202009%29.pdf. Acesso em: 27 maio 2024.
APA
Moser, C. A. S., Silvestrini, J. H., & Medeiros, M. A. F. de. (2009). Investigation of the aerodynamic noise radiation by subsonic jets at high Reynolds. In Proceedings. London, UK: Royal Aeronautical Society. Recuperado de https://repositorio.usp.br/directbitstream/d7f212bd-ec7e-4ceb-b423-b58cf4285ed4/trabalho%2062%20-%20%20Investigation%20of%20the%20aerodynamic%20noise%20radiation%20by%20subsonic%20jets%20at%20high%20Reynolds%20%28European%20air%20and%20space%20conference%2C%202009%29.pdf
NLM
Moser CAS, Silvestrini JH, Medeiros MAF de. Investigation of the aerodynamic noise radiation by subsonic jets at high Reynolds [Internet]. Proceedings. 2009 ;[citado 2024 maio 27 ] Available from: https://repositorio.usp.br/directbitstream/d7f212bd-ec7e-4ceb-b423-b58cf4285ed4/trabalho%2062%20-%20%20Investigation%20of%20the%20aerodynamic%20noise%20radiation%20by%20subsonic%20jets%20at%20high%20Reynolds%20%28European%20air%20and%20space%20conference%2C%202009%29.pdf
Vancouver
Moser CAS, Silvestrini JH, Medeiros MAF de. Investigation of the aerodynamic noise radiation by subsonic jets at high Reynolds [Internet]. Proceedings. 2009 ;[citado 2024 maio 27 ] Available from: https://repositorio.usp.br/directbitstream/d7f212bd-ec7e-4ceb-b423-b58cf4285ed4/trabalho%2062%20-%20%20Investigation%20of%20the%20aerodynamic%20noise%20radiation%20by%20subsonic%20jets%20at%20high%20Reynolds%20%28European%20air%20and%20space%20conference%2C%202009%29.pdf