Aircraft air inlet design optimization via surrogate-assisted evolutionary computation (2015)
Fonte: Evolutionary Multi-Criterion Optimization: 8th International Conference, EMO 2015, Guimarães, Portugal, March 29-April 1, 2015. Proceedings, Part II. Nome do evento: International Conference on Evolutionary Multi-Criterion Optimization - EMO. Unidade: IME
Assuntos: MECÂNICA DOS FLUÍDOS COMPUTACIONAL, ALGORITMOS, MATEMÁTICA APLICADA
ABNT
LOMBARDI, André e FERRARI, Denise Beatriz e SANTOS, Luis Carlos de Castro. Aircraft air inlet design optimization via surrogate-assisted evolutionary computation. 2015, Anais.. Cham: Springer, 2015. Disponível em: https://doi.org/10.1007/978-3-319-15892-1_21. Acesso em: 01 nov. 2024.APA
Lombardi, A., Ferrari, D. B., & Santos, L. C. de C. (2015). Aircraft air inlet design optimization via surrogate-assisted evolutionary computation. In Evolutionary Multi-Criterion Optimization: 8th International Conference, EMO 2015, Guimarães, Portugal, March 29-April 1, 2015. Proceedings, Part II. Cham: Springer. doi:10.1007/978-3-319-15892-1_21NLM
Lombardi A, Ferrari DB, Santos LC de C. Aircraft air inlet design optimization via surrogate-assisted evolutionary computation [Internet]. Evolutionary Multi-Criterion Optimization: 8th International Conference, EMO 2015, Guimarães, Portugal, March 29-April 1, 2015. Proceedings, Part II. 2015 ;[citado 2024 nov. 01 ] Available from: https://doi.org/10.1007/978-3-319-15892-1_21Vancouver
Lombardi A, Ferrari DB, Santos LC de C. Aircraft air inlet design optimization via surrogate-assisted evolutionary computation [Internet]. Evolutionary Multi-Criterion Optimization: 8th International Conference, EMO 2015, Guimarães, Portugal, March 29-April 1, 2015. Proceedings, Part II. 2015 ;[citado 2024 nov. 01 ] Available from: https://doi.org/10.1007/978-3-319-15892-1_21