The use of genetic algorithm for high-performance aerodynamic airfoil in compressible flow (2006)
- Authors:
- USP affiliated authors: SOUZA, LEANDRO FRANCO DE - ICMC ; MELLO, RODRIGO FERNANDES DE - ICMC
- Unidade: ICMC
- Assunto: MECÂNICA DOS FLUÍDOS COMPUTACIONAL
- Language: Inglês
- Imprenta:
- Source:
- Título do periódico: Proceedings of the ENCIT
- Conference titles: Brazilian Congress of Thermal Sciences and Engineering
-
ABNT
CUENCA, Rafael Gigena e SOUZA, Leandro Franco de e MELLO, Rodrigo Fernandes de. The use of genetic algorithm for high-performance aerodynamic airfoil in compressible flow. 2006, Anais.. Curitiba: ABCM, 2006. . Acesso em: 19 abr. 2024. -
APA
Cuenca, R. G., Souza, L. F. de, & Mello, R. F. de. (2006). The use of genetic algorithm for high-performance aerodynamic airfoil in compressible flow. In Proceedings of the ENCIT. Curitiba: ABCM. -
NLM
Cuenca RG, Souza LF de, Mello RF de. The use of genetic algorithm for high-performance aerodynamic airfoil in compressible flow. Proceedings of the ENCIT. 2006 ;[citado 2024 abr. 19 ] -
Vancouver
Cuenca RG, Souza LF de, Mello RF de. The use of genetic algorithm for high-performance aerodynamic airfoil in compressible flow. Proceedings of the ENCIT. 2006 ;[citado 2024 abr. 19 ] - The use of genetic algorithm for transonic airfoil optimization
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- Numerical simulation of a flow over a cylinder with immersed boundary technique in vorticity-velocity formulation
- Numerical propagation of one-dimensional waves with low-dispersion and low-dissipation methods
- The influence of spanwise wavelenght of Görtler vortices in heat transfer
- Compressible code verification using MMS
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