Accurate CFD measurements of vortex generators effects on a wing subject to shock-induced separation (2021)
- Authors:
- Autor USP: SANTOS, LUIS CARLOS DE CASTRO - IME
- Unidade: IME
- DOI: 10.2514/6.2021-1839
- Subjects: DINÂMICA DOS FLUÍDOS; MODELOS MATEMÁTICOS
- Language: Inglês
- Imprenta:
- Publisher: AIAA
- Publisher place: Reston, VA, USA
- Date published: 2021
- Source:
- Título: Proceedings
- Conference titles: AIAA Scitech Forum
- Este periódico é de assinatura
- Este artigo NÃO é de acesso aberto
- Cor do Acesso Aberto: closed
-
ABNT
FERRARI, Marcello et al. Accurate CFD measurements of vortex generators effects on a wing subject to shock-induced separation. 2021, Anais.. Reston, VA, USA: AIAA, 2021. Disponível em: https://doi.org/10.2514/6.2021-1839. Acesso em: 07 out. 2024. -
APA
Ferrari, M., Morais, K. C., Ferrari, D., Resende, O. C. de, & Santos, L. C. de C. (2021). Accurate CFD measurements of vortex generators effects on a wing subject to shock-induced separation. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2021-1839 -
NLM
Ferrari M, Morais KC, Ferrari D, Resende OC de, Santos LC de C. Accurate CFD measurements of vortex generators effects on a wing subject to shock-induced separation [Internet]. Proceedings. 2021 ;[citado 2024 out. 07 ] Available from: https://doi.org/10.2514/6.2021-1839 -
Vancouver
Ferrari M, Morais KC, Ferrari D, Resende OC de, Santos LC de C. Accurate CFD measurements of vortex generators effects on a wing subject to shock-induced separation [Internet]. Proceedings. 2021 ;[citado 2024 out. 07 ] Available from: https://doi.org/10.2514/6.2021-1839 - Aircraft air inlet design optimization via surrogate-assisted evolutionary computation
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Informações sobre o DOI: 10.2514/6.2021-1839 (Fonte: oaDOI API)
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