The effects of the number Mach and vorticity dynamic in asymmetric wake (2008)
- Authors:
- USP affiliated authors: MEDEIROS, MARCELLO AUGUSTO FARACO DE - EESC ; GENNARO, ELMER MATEUS - EESC ; GERMANOS, RICARDO ALBERTO COPPOLA - EESC
- Unidade: EESC
- Subjects: AERODINÂMICA DE AERONAVES; ENGENHARIA AERONÁUTICA
- Language: Inglês
- Imprenta:
- Publisher: ABCM
- Publisher place: Rio de Janeiro, RJ
- Date published: 2008
- Source:
- Título: Proceedings
- Conference titles: Brazilian Congress of Thermal Engineering and Sciences
-
ABNT
GENNARO, Elmer Mateus e GERMANOS, Ricardo Alberto Coppola e MEDEIROS, Marcello Augusto Faraco de. The effects of the number Mach and vorticity dynamic in asymmetric wake. 2008, Anais.. Rio de Janeiro, RJ: ABCM, 2008. Disponível em: https://repositorio.usp.br/directbitstream/f1377ed3-6241-4041-b51f-261f38e984e7/trabalho%2067%20-%20The%20effects%20of%20the%20Mach%20number%20and%20vorticity%20dynamic%20in%20asymmetric%20wake%20%28ENCIT%202008%29.pdf. Acesso em: 29 dez. 2025. -
APA
Gennaro, E. M., Germanos, R. A. C., & Medeiros, M. A. F. de. (2008). The effects of the number Mach and vorticity dynamic in asymmetric wake. In Proceedings. Rio de Janeiro, RJ: ABCM. Recuperado de https://repositorio.usp.br/directbitstream/f1377ed3-6241-4041-b51f-261f38e984e7/trabalho%2067%20-%20The%20effects%20of%20the%20Mach%20number%20and%20vorticity%20dynamic%20in%20asymmetric%20wake%20%28ENCIT%202008%29.pdf -
NLM
Gennaro EM, Germanos RAC, Medeiros MAF de. The effects of the number Mach and vorticity dynamic in asymmetric wake [Internet]. Proceedings. 2008 ;[citado 2025 dez. 29 ] Available from: https://repositorio.usp.br/directbitstream/f1377ed3-6241-4041-b51f-261f38e984e7/trabalho%2067%20-%20The%20effects%20of%20the%20Mach%20number%20and%20vorticity%20dynamic%20in%20asymmetric%20wake%20%28ENCIT%202008%29.pdf -
Vancouver
Gennaro EM, Germanos RAC, Medeiros MAF de. The effects of the number Mach and vorticity dynamic in asymmetric wake [Internet]. Proceedings. 2008 ;[citado 2025 dez. 29 ] Available from: https://repositorio.usp.br/directbitstream/f1377ed3-6241-4041-b51f-261f38e984e7/trabalho%2067%20-%20The%20effects%20of%20the%20Mach%20number%20and%20vorticity%20dynamic%20in%20asymmetric%20wake%20%28ENCIT%202008%29.pdf - Numerical simulation of a strongly spanwise modulated wavetrain in a compressible mixing layer
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- Natural transition in plane poiseuille flow
- Development of a code for biglobal linear stability analysis of compressible flows: application to leading-edge boundary layer
- Sparse techniques in global flow instability with application to compressible leading-edge flow
- Linear instability of orthogonal compressible leading-edge boundary layer flow
- Nonlinear interaction between wavepackets in plane poiseuille flow
- On the vortex pairing aeroacoustics of a 2D mixing layer under temporal development
- Wavepackets in a compressible subsonic adverse pressure gradient boundary layer
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