Nonlinear geometric decomposition of airfoils into the thickness and camber contributions (2024)
Source: Meccanica. Unidade: EESC
Subjects: AEROFÓLIOS, MÉTODO DE DIFERENÇAS FINITAS, ENGENHARIA MECÂNICA
ABNT
TORRES, George Lucas Souto e MARQUES, Flavio Donizeti. Nonlinear geometric decomposition of airfoils into the thickness and camber contributions. Meccanica, v. 59, p. 889-907, 2024Tradução . . Disponível em: https://dx.doi.org/10.1007/s11012-024-01801-6. Acesso em: 06 set. 2024.APA
Torres, G. L. S., & Marques, F. D. (2024). Nonlinear geometric decomposition of airfoils into the thickness and camber contributions. Meccanica, 59, 889-907. doi:10.1007/s11012-024-01801-6NLM
Torres GLS, Marques FD. Nonlinear geometric decomposition of airfoils into the thickness and camber contributions [Internet]. Meccanica. 2024 ; 59 889-907.[citado 2024 set. 06 ] Available from: https://dx.doi.org/10.1007/s11012-024-01801-6Vancouver
Torres GLS, Marques FD. Nonlinear geometric decomposition of airfoils into the thickness and camber contributions [Internet]. Meccanica. 2024 ; 59 889-907.[citado 2024 set. 06 ] Available from: https://dx.doi.org/10.1007/s11012-024-01801-6