Bravo Mosquera, Pedro David; Cerón Muñoz, Hernán Darío 
; Catalano, Fernando Martini
Fonte: Aerospace. Unidade: EESC
Assuntos: AERODINÂMICA DE AERONAVES, TÚNEIS DE VENTO, ENGENHARIA AERONÁUTICA
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BRAVO MOSQUERA, Pedro David e CERÓN MUÑOZ, Hernán Darío e CATALANO, Fernando Martini. Potential propulsive and aerodynamic benefits of a new aircraft concept: a low-speed experimental study. Aerospace, v. 10, n. 7, p. 1-26, 2023Tradução . . Disponível em: https://doi.org/10.3390/aerospace10070651. Acesso em: 14 nov. 2024.APA
Bravo Mosquera, P. D., Cerón Muñoz, H. D., & Catalano, F. M. (2023). Potential propulsive and aerodynamic benefits of a new aircraft concept: a low-speed experimental study. Aerospace, 10( 7), 1-26. doi:10.3390/aerospace10070651NLM
Bravo Mosquera PD, Cerón Muñoz HD, Catalano FM. Potential propulsive and aerodynamic benefits of a new aircraft concept: a low-speed experimental study [Internet]. Aerospace. 2023 ; 10( 7): 1-26.[citado 2024 nov. 14 ] Available from: https://doi.org/10.3390/aerospace10070651Vancouver
Bravo Mosquera PD, Cerón Muñoz HD, Catalano FM. Potential propulsive and aerodynamic benefits of a new aircraft concept: a low-speed experimental study [Internet]. Aerospace. 2023 ; 10( 7): 1-26.[citado 2024 nov. 14 ] Available from: https://doi.org/10.3390/aerospace10070651
