Vaca Rios, John Jairo 
; Cerón Muñoz, Hernán Darío
Source: Aerospace Science and Technology. Unidade: EESC
Subjects: AERODINÂMICA DE AERONAVES, PROPULSÃO DE AERONAVES, DINÂMICA DOS FLUÍDOS COMPUTACIONAL, ENGENHARIA AERONÁUTICA
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VACA RIOS, John Jairo e CERÓN MUÑOZ, Hernán Darío. A proposed methodology for diverterless supersonic inlet aerodynamic integration with a generic forebody. Aerospace Science and Technology, v. 161, p. 1-14, 2025Tradução . . Disponível em: http://dx.doi.org/10.1016/j.ast.2025.110135. Acesso em: 23 fev. 2026.APA
Vaca Rios, J. J., & Cerón Muñoz, H. D. (2025). A proposed methodology for diverterless supersonic inlet aerodynamic integration with a generic forebody. Aerospace Science and Technology, 161, 1-14. doi:10.1016/j.ast.2025.110135NLM
Vaca Rios JJ, Cerón Muñoz HD. A proposed methodology for diverterless supersonic inlet aerodynamic integration with a generic forebody [Internet]. Aerospace Science and Technology. 2025 ; 161 1-14.[citado 2026 fev. 23 ] Available from: http://dx.doi.org/10.1016/j.ast.2025.110135Vancouver
Vaca Rios JJ, Cerón Muñoz HD. A proposed methodology for diverterless supersonic inlet aerodynamic integration with a generic forebody [Internet]. Aerospace Science and Technology. 2025 ; 161 1-14.[citado 2026 fev. 23 ] Available from: http://dx.doi.org/10.1016/j.ast.2025.110135
