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Trabalho de evento
A study of the sources of slat noise using proper orthogonal decomposition (2013)
Souza, Daniel Sampaio; Rodriguez, Daniel; Medeiros, Marcello Augusto Faraco de
Source: Proceedings. Conference titles: AIAA/CEAS Aeroacoustics Conference. Unidade: EESC
Subjects: SLATS, AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA
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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: 19 set. 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 set. 19 ] 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 set. 19 ] 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
Trabalho de evento
Method for aeroacoustic analysis in asymmetric wake flow (2013)
Mathias, Marlon Sproesser; Medeiros, Marcello Augusto Faraco de
Source: Anais. Conference titles: International Congress of Mechanical Engineering - COBEM. Unidade: EESC
Assunto: ENGENHARIA AERONÁUTICA
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ABNT
MATHIAS, Marlon Sproesser e MEDEIROS, Marcello Augusto Faraco de. Method for aeroacoustic analysis in asymmetric wake flow. 2013, Anais.. Rio de Janeiro, RJ: ABCM, 2013. . Acesso em: 19 set. 2024.
APA
Mathias, M. S., & Medeiros, M. A. F. de. (2013). Method for aeroacoustic analysis in asymmetric wake flow. In Anais. Rio de Janeiro, RJ: ABCM.
NLM
Mathias MS, Medeiros MAF de. Method for aeroacoustic analysis in asymmetric wake flow. Anais. 2013 ;[citado 2024 set. 19 ]
Vancouver
Mathias MS, Medeiros MAF de. Method for aeroacoustic analysis in asymmetric wake flow. Anais. 2013 ;[citado 2024 set. 19 ]
Artigo de periodico
On the controversy regarding the effect of flow shear on the Strouhal number of cylinder vortex shedding (2013)
Gennaro, Elmer Mateus; Colaciti, Alysson Kennerly; Medeiros, Marcello Augusto Faraco de
Source: Aerospace Science and Technology. Unidade: EESC
Subjects: HIDRODINÂMICA, EQUAÇÕES
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
GENNARO, Elmer Mateus e COLACITI, Alysson Kennerly e MEDEIROS, Marcello Augusto Faraco de. On the controversy regarding the effect of flow shear on the Strouhal number of cylinder vortex shedding. Aerospace Science and Technology, v. 29, n. 1, p. 313-320, 2013Tradução . . Disponível em: https://doi.org/10.1016/j.ast.2013.04.002. Acesso em: 19 set. 2024.
APA
Gennaro, E. M., Colaciti, A. K., & Medeiros, M. A. F. de. (2013). On the controversy regarding the effect of flow shear on the Strouhal number of cylinder vortex shedding. Aerospace Science and Technology, 29( 1), 313-320. doi:10.1016/j.ast.2013.04.002
NLM
Gennaro EM, Colaciti AK, Medeiros MAF de. On the controversy regarding the effect of flow shear on the Strouhal number of cylinder vortex shedding [Internet]. Aerospace Science and Technology. 2013 ; 29( 1): 313-320.[citado 2024 set. 19 ] Available from: https://doi.org/10.1016/j.ast.2013.04.002
Vancouver
Gennaro EM, Colaciti AK, Medeiros MAF de. On the controversy regarding the effect of flow shear on the Strouhal number of cylinder vortex shedding [Internet]. Aerospace Science and Technology. 2013 ; 29( 1): 313-320.[citado 2024 set. 19 ] Available from: https://doi.org/10.1016/j.ast.2013.04.002
Trabalho de evento
Effect of Mach number on linear stability of lid-driven cavity flows (2013)
Bergamo, Leandro Fernandes; Gennaro, Elmer Mateus; Medeiros, Marcello Augusto Faraco de
Source: Proceedings. Conference titles: AIAA Fluid Dynamics Conference & Exhibit. Unidade: EESC
Subjects: AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA
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: 19 set. 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 set. 19 ] 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 set. 19 ] 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
Trabalho de evento
On detrimental effects of excrescences on the slat noise (2012)
Bandle, Lukas; Souza, Daniel Sampaio; Simões, Leandro Guilherme Crenite; Medeiros, Marcello Augusto Faraco de
Source: Proceedings. Conference titles: AIAA/CEAS Aeroacoustics Conference. Unidade: EESC
Subjects: AEROACÚSTICA, SLATS, ENGENHARIA AERONÁUTICA
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: 19 set. 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 set. 19 ] 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 set. 19 ] 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
Trabalho de evento
Non-conservative implicit large-eddy simulation method for predicting the noise radiated by subsonic jets (2012)
Moser, Carlos A. S.; Medeiros, Marcello Augusto Faraco de
Source: Proceedings. Conference titles: AIAA/CEAS Aeroacoustics Conference. Unidade: EESC
Subjects: AEROACÚSTICA, ENGENHARIA AERONÁUTICA
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: 19 set. 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 set. 19 ] 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 set. 19 ] 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
Trabalho de evento
High-order and high-accurate immersed interface method for uid dynamics (2012)
Coutinho, Eduardo de Castro; Medeiros, Marcello Augusto Faraco de
Source: Proceedings. Conference titles: World Congress on Computational Mechanics - WCCM. Unidade: EESC
Subjects: AEROACÚSTICA, ENGENHARIA AERONÁUTICA
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: 19 set. 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 set. 19 ] 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 set. 19 ] 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
Trabalho de evento
Wavepackets in a compressible subsonic adverse pressure gradient boundary layer (2012)
Gennaro, Elmer Mateus; Bergamo, Leandro Fernandes; Medeiros, Marcello Augusto Faraco de
Source: Proceedings. Conference titles: AIAA Fluid Dynamics Conference & Exhibit. Unidade: EESC
Subjects: MECÂNICA DOS FLUÍDOS COMPUTACIONAL, ENGENHARIA AERONÁUTICA
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: 19 set. 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 set. 19 ]
Vancouver
Gennaro EM, Bergamo LF, Medeiros MAF de. Wavepackets in a compressible subsonic adverse pressure gradient boundary layer. Proceedings. 2012 ;[citado 2024 set. 19 ]
Trabalho de evento
Large-eddy simulation of noise radiated by a mach 0.9 round jet at high reynolds number (2011)
Moser, Carlos Anissem Soares; Medeiros, Marcello Augusto Faraco de ; Silvestrini, Jorge Hugo
Source: Proceedings of COBEM. Conference titles: International Congress of Mechanical Engineering - COBEM. Unidade: EESC
Subjects: AEROACÚSTICA, AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
MOSER, Carlos Anissem Soares e MEDEIROS, Marcello Augusto Faraco de e SILVESTRINI, Jorge Hugo. Large-eddy simulation of noise radiated by a mach 0.9 round jet at high reynolds number. 2011, Anais.. Rio de Janeiro, RJ: ABCM, 2011. Disponível em: https://repositorio.usp.br/directbitstream/270f240d-8f2a-49dd-ae6b-55a78f1b1d2b/trabalho%2045%20-%20Large-eddy%20simulation%20of%20noise%20radiated%20by%20a%20Mach%200.9%20round%20jet%20at%20high%20Reynolds%20number%20%28COBEM%202011%29.pdf. Acesso em: 19 set. 2024.
APA
Moser, C. A. S., Medeiros, M. A. F. de, & Silvestrini, J. H. (2011). Large-eddy simulation of noise radiated by a mach 0.9 round jet at high reynolds number. In Proceedings of COBEM. Rio de Janeiro, RJ: ABCM. Recuperado de https://repositorio.usp.br/directbitstream/270f240d-8f2a-49dd-ae6b-55a78f1b1d2b/trabalho%2045%20-%20Large-eddy%20simulation%20of%20noise%20radiated%20by%20a%20Mach%200.9%20round%20jet%20at%20high%20Reynolds%20number%20%28COBEM%202011%29.pdf
NLM
Moser CAS, Medeiros MAF de, Silvestrini JH. Large-eddy simulation of noise radiated by a mach 0.9 round jet at high reynolds number [Internet]. Proceedings of COBEM. 2011 ;[citado 2024 set. 19 ] Available from: https://repositorio.usp.br/directbitstream/270f240d-8f2a-49dd-ae6b-55a78f1b1d2b/trabalho%2045%20-%20Large-eddy%20simulation%20of%20noise%20radiated%20by%20a%20Mach%200.9%20round%20jet%20at%20high%20Reynolds%20number%20%28COBEM%202011%29.pdf
Vancouver
Moser CAS, Medeiros MAF de, Silvestrini JH. Large-eddy simulation of noise radiated by a mach 0.9 round jet at high reynolds number [Internet]. Proceedings of COBEM. 2011 ;[citado 2024 set. 19 ] Available from: https://repositorio.usp.br/directbitstream/270f240d-8f2a-49dd-ae6b-55a78f1b1d2b/trabalho%2045%20-%20Large-eddy%20simulation%20of%20noise%20radiated%20by%20a%20Mach%200.9%20round%20jet%20at%20high%20Reynolds%20number%20%28COBEM%202011%29.pdf
Trabalho de evento
Direct numerical simulation of a transitional bubble in a compressible boundary layer (2011)
Moreto, José Roberto; Gennaro, Elmer Mateus ; Medeiros, Marcello Augusto Faraco de
Source: Proceedings of COBEM. Conference titles: International Congress of Mechanical Engineering - COBEM. Unidade: EESC
Subjects: AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
MORETO, José Roberto e GENNARO, Elmer Mateus e MEDEIROS, Marcello Augusto Faraco de. Direct numerical simulation of a transitional bubble in a compressible boundary layer. 2011, Anais.. Rio de Janeiro, RJ: ABCM, 2011. Disponível em: https://repositorio.usp.br/directbitstream/94d2a140-bd0c-487f-bc64-043d8d54e50c/trabalho%20DIRECT%20NUMERICAL%20SIMULATION%20OF%20A%20TRANSITIONAL%20BUBBLE%20IN%20A%20COMPRESSIBLE%20BOUNDARY%20LAYER%20%28COBEM%202011%29.pdf. Acesso em: 19 set. 2024.
APA
Moreto, J. R., Gennaro, E. M., & Medeiros, M. A. F. de. (2011). Direct numerical simulation of a transitional bubble in a compressible boundary layer. In Proceedings of COBEM. Rio de Janeiro, RJ: ABCM. Recuperado de https://repositorio.usp.br/directbitstream/94d2a140-bd0c-487f-bc64-043d8d54e50c/trabalho%20DIRECT%20NUMERICAL%20SIMULATION%20OF%20A%20TRANSITIONAL%20BUBBLE%20IN%20A%20COMPRESSIBLE%20BOUNDARY%20LAYER%20%28COBEM%202011%29.pdf
NLM
Moreto JR, Gennaro EM, Medeiros MAF de. Direct numerical simulation of a transitional bubble in a compressible boundary layer [Internet]. Proceedings of COBEM. 2011 ;[citado 2024 set. 19 ] Available from: https://repositorio.usp.br/directbitstream/94d2a140-bd0c-487f-bc64-043d8d54e50c/trabalho%20DIRECT%20NUMERICAL%20SIMULATION%20OF%20A%20TRANSITIONAL%20BUBBLE%20IN%20A%20COMPRESSIBLE%20BOUNDARY%20LAYER%20%28COBEM%202011%29.pdf
Vancouver
Moreto JR, Gennaro EM, Medeiros MAF de. Direct numerical simulation of a transitional bubble in a compressible boundary layer [Internet]. Proceedings of COBEM. 2011 ;[citado 2024 set. 19 ] Available from: https://repositorio.usp.br/directbitstream/94d2a140-bd0c-487f-bc64-043d8d54e50c/trabalho%20DIRECT%20NUMERICAL%20SIMULATION%20OF%20A%20TRANSITIONAL%20BUBBLE%20IN%20A%20COMPRESSIBLE%20BOUNDARY%20LAYER%20%28COBEM%202011%29.pdf
Trabalho de evento
On the small effect of boundary layer thicknesses on slat noise (2011)
Simões, Leandro Guilherme Crenite; Souza, Daniel Sampaio; Medeiros, Marcello Augusto Faraco de
Source: Proceedings. Conference titles: AIAA/CEAS Aeroacoustics Conference. Unidade: EESC
Subjects: AEROACÚSTICA, FUSELAGEM DE AERONAVES, ENGENHARIA AERONÁUTICA
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: 19 set. 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 set. 19 ] 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 set. 19 ] 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
Trabalho de evento-resumo
Uso de atuadores piezelétricos para o controle de escoamento em aerofólios (2011)
Alarcon, Danilo Sartori; Medeiros, Marcello Augusto Faraco de; De Marqui Júnior, Carlos
Source: Resumos. Conference titles: Simpósio Internacional de Iniciação Científica da Universidade de São Paulo - SIICUSP. Unidade: EESC
Subjects: AERODINÂMICA DE AERONAVES, ATUADORES PIEZELÉTRICOS, ESCOAMENTO (CONTROLE)
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
ALARCON, Danilo Sartori e MEDEIROS, Marcello Augusto Faraco de e DE MARQUI JÚNIOR, Carlos. Uso de atuadores piezelétricos para o controle de escoamento em aerofólios. 2011, Anais.. São Paulo: USP/Pró-Reitoria de Pesquisa, 2011. Disponível em: https://sistemas.usp.br/siicusp/cdOnlineTrabalhoVisualizarResumo?numeroInscricaoTrabalho=2876&numeroEdicao=19. Acesso em: 19 set. 2024.
APA
Alarcon, D. S., Medeiros, M. A. F. de, & De Marqui Júnior, C. (2011). Uso de atuadores piezelétricos para o controle de escoamento em aerofólios. In Resumos. São Paulo: USP/Pró-Reitoria de Pesquisa. Recuperado de https://sistemas.usp.br/siicusp/cdOnlineTrabalhoVisualizarResumo?numeroInscricaoTrabalho=2876&numeroEdicao=19
NLM
Alarcon DS, Medeiros MAF de, De Marqui Júnior C. Uso de atuadores piezelétricos para o controle de escoamento em aerofólios [Internet]. Resumos. 2011 ;[citado 2024 set. 19 ] Available from: https://sistemas.usp.br/siicusp/cdOnlineTrabalhoVisualizarResumo?numeroInscricaoTrabalho=2876&numeroEdicao=19
Vancouver
Alarcon DS, Medeiros MAF de, De Marqui Júnior C. Uso de atuadores piezelétricos para o controle de escoamento em aerofólios [Internet]. Resumos. 2011 ;[citado 2024 set. 19 ] Available from: https://sistemas.usp.br/siicusp/cdOnlineTrabalhoVisualizarResumo?numeroInscricaoTrabalho=2876&numeroEdicao=19
Trabalho de evento
Computação do ruído aerodinâmico irradiado por um jato subsônico a número de Reynolds elevado (2011)
Moser, Carlos Anissem Soares; Medeiros, Marcello Augusto Faraco de ; Silvestrini, Jorge Hugo
Source: Actas. Conference titles: Congresso Ibero-Americano em Engenharia Mecânica - CIBEM. Unidade: EESC
Subjects: AEROACÚSTICA, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
MOSER, Carlos Anissem Soares e MEDEIROS, Marcello Augusto Faraco de e SILVESTRINI, Jorge Hugo. Computação do ruído aerodinâmico irradiado por um jato subsônico a número de Reynolds elevado. 2011, Anais.. Porto, Portugal: FEUP, 2011. Disponível em: https://repositorio.usp.br/directbitstream/4b589953-5b16-4618-8d96-302171131a28/trabalho%2044%20-%20COMPUTA%C3%87%C3%83O%20DO%20RU%C3%8DDO%20AERODIN%20MICO%20IRRADIADO%20POR%20UM%20JATO%20SUBS%C3%94NICO%20A%20N%C3%9AMERO%20DE%20REYNOLDS%20ELEVADO%20%28CIBEM10%2C%202011%29.pdf. Acesso em: 19 set. 2024.
APA
Moser, C. A. S., Medeiros, M. A. F. de, & Silvestrini, J. H. (2011). Computação do ruído aerodinâmico irradiado por um jato subsônico a número de Reynolds elevado. In Actas. Porto, Portugal: FEUP. Recuperado de https://repositorio.usp.br/directbitstream/4b589953-5b16-4618-8d96-302171131a28/trabalho%2044%20-%20COMPUTA%C3%87%C3%83O%20DO%20RU%C3%8DDO%20AERODIN%20MICO%20IRRADIADO%20POR%20UM%20JATO%20SUBS%C3%94NICO%20A%20N%C3%9AMERO%20DE%20REYNOLDS%20ELEVADO%20%28CIBEM10%2C%202011%29.pdf
NLM
Moser CAS, Medeiros MAF de, Silvestrini JH. Computação do ruído aerodinâmico irradiado por um jato subsônico a número de Reynolds elevado [Internet]. Actas. 2011 ;[citado 2024 set. 19 ] Available from: https://repositorio.usp.br/directbitstream/4b589953-5b16-4618-8d96-302171131a28/trabalho%2044%20-%20COMPUTA%C3%87%C3%83O%20DO%20RU%C3%8DDO%20AERODIN%20MICO%20IRRADIADO%20POR%20UM%20JATO%20SUBS%C3%94NICO%20A%20N%C3%9AMERO%20DE%20REYNOLDS%20ELEVADO%20%28CIBEM10%2C%202011%29.pdf
Vancouver
Moser CAS, Medeiros MAF de, Silvestrini JH. Computação do ruído aerodinâmico irradiado por um jato subsônico a número de Reynolds elevado [Internet]. Actas. 2011 ;[citado 2024 set. 19 ] Available from: https://repositorio.usp.br/directbitstream/4b589953-5b16-4618-8d96-302171131a28/trabalho%2044%20-%20COMPUTA%C3%87%C3%83O%20DO%20RU%C3%8DDO%20AERODIN%20MICO%20IRRADIADO%20POR%20UM%20JATO%20SUBS%C3%94NICO%20A%20N%C3%9AMERO%20DE%20REYNOLDS%20ELEVADO%20%28CIBEM10%2C%202011%29.pdf
Trabalho de evento
Linear instability of orthogonal compressible leading-edge boundary layer flow (2011)
Gennaro, Elmer Mateus; Rodríguez, D.; Medeiros, Marcello Augusto Faraco de ; Theofilis, V.
Source: Papers. Conference titles: AIAA Theoretical Fluid Mechanics Conference. Unidade: EESC
Subjects: EQUAÇÕES DE NAVIER-STOKES, MECÂNICA DOS FLUÍDOS COMPUTACIONAL, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
GENNARO, Elmer Mateus et al. Linear instability of orthogonal compressible leading-edge boundary layer flow. 2011, Anais.. Reston, VA, USA: AIAA, 2011. . Acesso em: 19 set. 2024.
APA
Gennaro, E. M., Rodríguez, D., Medeiros, M. A. F. de, & Theofilis, V. (2011). Linear instability of orthogonal compressible leading-edge boundary layer flow. In Papers. Reston, VA, USA: AIAA.
NLM
Gennaro EM, Rodríguez D, Medeiros MAF de, Theofilis V. Linear instability of orthogonal compressible leading-edge boundary layer flow. Papers. 2011 ;[citado 2024 set. 19 ]
Vancouver
Gennaro EM, Rodríguez D, Medeiros MAF de, Theofilis V. Linear instability of orthogonal compressible leading-edge boundary layer flow. Papers. 2011 ;[citado 2024 set. 19 ]
Trabalho de evento-resumo
Métodos de ensaios de aeroacústica para turbinas eólicas (2011)
Hortencio, Marcos Eduardo de Oliveira; Medeiros, Marcello Augusto Faraco de
Source: Resumos. Conference titles: Simpósio Internacional de Iniciação Científica da Universidade de São Paulo - SIICUSP. Unidade: EESC
Subjects: AERODINÂMICA DE AERONAVES, TURBINAS
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
HORTENCIO, Marcos Eduardo de Oliveira e MEDEIROS, Marcello Augusto Faraco de. Métodos de ensaios de aeroacústica para turbinas eólicas. 2011, Anais.. São Paulo: USP/Pró-Reitoria de Pesquisa, 2011. Disponível em: https://sistemas.usp.br/siicusp/cdOnlineTrabalhoVisualizarResumo?numeroInscricaoTrabalho=1402&numeroEdicao=19. Acesso em: 19 set. 2024.
APA
Hortencio, M. E. de O., & Medeiros, M. A. F. de. (2011). Métodos de ensaios de aeroacústica para turbinas eólicas. In Resumos. São Paulo: USP/Pró-Reitoria de Pesquisa. Recuperado de https://sistemas.usp.br/siicusp/cdOnlineTrabalhoVisualizarResumo?numeroInscricaoTrabalho=1402&numeroEdicao=19
NLM
Hortencio ME de O, Medeiros MAF de. Métodos de ensaios de aeroacústica para turbinas eólicas [Internet]. Resumos. 2011 ;[citado 2024 set. 19 ] Available from: https://sistemas.usp.br/siicusp/cdOnlineTrabalhoVisualizarResumo?numeroInscricaoTrabalho=1402&numeroEdicao=19
Vancouver
Hortencio ME de O, Medeiros MAF de. Métodos de ensaios de aeroacústica para turbinas eólicas [Internet]. Resumos. 2011 ;[citado 2024 set. 19 ] Available from: https://sistemas.usp.br/siicusp/cdOnlineTrabalhoVisualizarResumo?numeroInscricaoTrabalho=1402&numeroEdicao=19
Trabalho de evento
A study to investigate wind tunnel background noise for the purpose of aeroacoustic beamforming (2011)
Pagani Júnior, Carlos do Carmo; Costa, Leandro; Medeiros, Marcello Augusto Faraco de
Source: Proceedings of COBEM. Conference titles: International Congress of Mechanical Engineering - COBEM. Unidade: EESC
Subjects: AEROACÚSTICA, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
PAGANI JÚNIOR, Carlos do Carmo e COSTA, Leandro e MEDEIROS, Marcello Augusto Faraco de. A study to investigate wind tunnel background noise for the purpose of aeroacoustic beamforming. 2011, Anais.. Rio de Janeiro, RJ: ABCM, 2011. Disponível em: https://repositorio.usp.br/directbitstream/5147c48a-537d-491b-ada3-7cbb02fdcd7a/trabalho%2046%20-%20A%20study%20to%20investigate%20wind%20tunnel%20background%20noise%20for%20the%20purpose%20of%20aeroacoustic%20beamforming%20%28COBEM%202011%29.pdf. Acesso em: 19 set. 2024.
APA
Pagani Júnior, C. do C., Costa, L., & Medeiros, M. A. F. de. (2011). A study to investigate wind tunnel background noise for the purpose of aeroacoustic beamforming. In Proceedings of COBEM. Rio de Janeiro, RJ: ABCM. Recuperado de https://repositorio.usp.br/directbitstream/5147c48a-537d-491b-ada3-7cbb02fdcd7a/trabalho%2046%20-%20A%20study%20to%20investigate%20wind%20tunnel%20background%20noise%20for%20the%20purpose%20of%20aeroacoustic%20beamforming%20%28COBEM%202011%29.pdf
NLM
Pagani Júnior C do C, Costa L, Medeiros MAF de. A study to investigate wind tunnel background noise for the purpose of aeroacoustic beamforming [Internet]. Proceedings of COBEM. 2011 ;[citado 2024 set. 19 ] Available from: https://repositorio.usp.br/directbitstream/5147c48a-537d-491b-ada3-7cbb02fdcd7a/trabalho%2046%20-%20A%20study%20to%20investigate%20wind%20tunnel%20background%20noise%20for%20the%20purpose%20of%20aeroacoustic%20beamforming%20%28COBEM%202011%29.pdf
Vancouver
Pagani Júnior C do C, Costa L, Medeiros MAF de. A study to investigate wind tunnel background noise for the purpose of aeroacoustic beamforming [Internet]. Proceedings of COBEM. 2011 ;[citado 2024 set. 19 ] Available from: https://repositorio.usp.br/directbitstream/5147c48a-537d-491b-ada3-7cbb02fdcd7a/trabalho%2046%20-%20A%20study%20to%20investigate%20wind%20tunnel%20background%20noise%20for%20the%20purpose%20of%20aeroacoustic%20beamforming%20%28COBEM%202011%29.pdf
Trabalho de evento
Steady aerodynamic simulation of a high-lift geometry by meams of a hybrid euler/integral boundary layer code (2011)
Souza, Daniel Sampaio; Medeiros, Marcello Augusto Faraco de
Source: Proceedings of COBEM. Conference titles: International Congress of Mechanical Engineering - COBEM. Unidade: EESC
Subjects: AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
SOUZA, Daniel Sampaio e MEDEIROS, Marcello Augusto Faraco de. Steady aerodynamic simulation of a high-lift geometry by meams of a hybrid euler/integral boundary layer code. 2011, Anais.. Rio de Janeiro, RJ: ABCM, 2011. Disponível em: https://repositorio.usp.br/directbitstream/6e49e879-a73f-4d4f-9de3-7fab0c7cc644/trabalho%2047%20-%20Steady%20Aerodynamic%20Simulation%20of%20a%20High-Lift%20Geometry%20by%20Means%20of%20a%20Hybrid%20Euler-IBL%20Code%20%28COBEM%202011%29.pdf. Acesso em: 19 set. 2024.
APA
Souza, D. S., & Medeiros, M. A. F. de. (2011). Steady aerodynamic simulation of a high-lift geometry by meams of a hybrid euler/integral boundary layer code. In Proceedings of COBEM. Rio de Janeiro, RJ: ABCM. Recuperado de https://repositorio.usp.br/directbitstream/6e49e879-a73f-4d4f-9de3-7fab0c7cc644/trabalho%2047%20-%20Steady%20Aerodynamic%20Simulation%20of%20a%20High-Lift%20Geometry%20by%20Means%20of%20a%20Hybrid%20Euler-IBL%20Code%20%28COBEM%202011%29.pdf
NLM
Souza DS, Medeiros MAF de. Steady aerodynamic simulation of a high-lift geometry by meams of a hybrid euler/integral boundary layer code [Internet]. Proceedings of COBEM. 2011 ;[citado 2024 set. 19 ] Available from: https://repositorio.usp.br/directbitstream/6e49e879-a73f-4d4f-9de3-7fab0c7cc644/trabalho%2047%20-%20Steady%20Aerodynamic%20Simulation%20of%20a%20High-Lift%20Geometry%20by%20Means%20of%20a%20Hybrid%20Euler-IBL%20Code%20%28COBEM%202011%29.pdf
Vancouver
Souza DS, Medeiros MAF de. Steady aerodynamic simulation of a high-lift geometry by meams of a hybrid euler/integral boundary layer code [Internet]. Proceedings of COBEM. 2011 ;[citado 2024 set. 19 ] Available from: https://repositorio.usp.br/directbitstream/6e49e879-a73f-4d4f-9de3-7fab0c7cc644/trabalho%2047%20-%20Steady%20Aerodynamic%20Simulation%20of%20a%20High-Lift%20Geometry%20by%20Means%20of%20a%20Hybrid%20Euler-IBL%20Code%20%28COBEM%202011%29.pdf
Trabalho de evento
The update process and characterization of the Sao Paulo University wind-tunnel for aeroacoustics testing (2010)
Santana, Leandro Dantas; Catalano, Fernando Martini ; Medeiros, Marcello Augusto Faraco de ; Carmo, Micael
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: AEROACÚSTICA, TÚNEIS DE VENTO, ENGENHARIA AERONÁUTICA
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: 19 set. 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 set. 19 ]
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 set. 19 ]
Artigo de periodico
Verification of a mixed high-order accurate DNS code for laminar turbulent transition by the method of manufactured solutions (2010)
Silva, Homero Ghioti da; Souza, Leandro Franco de ; Medeiros, Marcello Augusto Faraco de
Source: International Journal for Numerical Methods in Fluids. Unidade: EESC
Subjects: HIDRODINÂMICA, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
SILVA, Homero Ghioti da e SOUZA, Leandro Franco de e MEDEIROS, Marcello Augusto Faraco de. Verification of a mixed high-order accurate DNS code for laminar turbulent transition by the method of manufactured solutions. International Journal for Numerical Methods in Fluids, v. 64, p. 336-354, 2010Tradução . . Disponível em: https://doi.org/10.1002/fld.2156. Acesso em: 19 set. 2024.
APA
Silva, H. G. da, Souza, L. F. de, & Medeiros, M. A. F. de. (2010). Verification of a mixed high-order accurate DNS code for laminar turbulent transition by the method of manufactured solutions. International Journal for Numerical Methods in Fluids, 64, 336-354. doi:10.1002/fld.2156
NLM
Silva HG da, Souza LF de, Medeiros MAF de. Verification of a mixed high-order accurate DNS code for laminar turbulent transition by the method of manufactured solutions [Internet]. International Journal for Numerical Methods in Fluids. 2010 ; 64 336-354.[citado 2024 set. 19 ] Available from: https://doi.org/10.1002/fld.2156
Vancouver
Silva HG da, Souza LF de, Medeiros MAF de. Verification of a mixed high-order accurate DNS code for laminar turbulent transition by the method of manufactured solutions [Internet]. International Journal for Numerical Methods in Fluids. 2010 ; 64 336-354.[citado 2024 set. 19 ] Available from: https://doi.org/10.1002/fld.2156
Artigo de periodico
Verification of a mixed high-order accurate DNS code for laminar turbulent transition by the method of manufactured solutions (2010)
Silva, H G; Souza, Leandro Franco de ; Medeiros, M A F
Source: International Journal for Numerical Mehtods in Fluids. Unidades: ICMC, EESC
Assunto: MECÂNICA DOS FLUÍDOS COMPUTACIONAL
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
SILVA, H G e SOUZA, Leandro Franco de e MEDEIROS, M A F. Verification of a mixed high-order accurate DNS code for laminar turbulent transition by the method of manufactured solutions. International Journal for Numerical Mehtods in Fluids, v. 64, n. 3, p. 336-354, 2010Tradução . . Disponível em: https://doi.org/10.1002/fld.2156. Acesso em: 19 set. 2024.
APA
Silva, H. G., Souza, L. F. de, & Medeiros, M. A. F. (2010). Verification of a mixed high-order accurate DNS code for laminar turbulent transition by the method of manufactured solutions. International Journal for Numerical Mehtods in Fluids, 64( 3), 336-354. doi:10.1002/fld.2156
NLM
Silva HG, Souza LF de, Medeiros MAF. Verification of a mixed high-order accurate DNS code for laminar turbulent transition by the method of manufactured solutions [Internet]. International Journal for Numerical Mehtods in Fluids. 2010 ;64( 3): 336-354.[citado 2024 set. 19 ] Available from: https://doi.org/10.1002/fld.2156
Vancouver
Silva HG, Souza LF de, Medeiros MAF. Verification of a mixed high-order accurate DNS code for laminar turbulent transition by the method of manufactured solutions [Internet]. International Journal for Numerical Mehtods in Fluids. 2010 ;64( 3): 336-354.[citado 2024 set. 19 ] Available from: https://doi.org/10.1002/fld.2156

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