Bravo Mosquera, Pedro David; Cerón Muñoz, Hernán Darío 
; Catalano, Fernando Martini
Source: Proceedings. Conference titles: AIAA Propulsion and Energy Forum. Unidade: EESC
Subjects: ENGENHARIA AERONÁUTICA, ASAS DE AERONAVES, AERODINÂMICA DE AERONAVES
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BRAVO MOSQUERA, Pedro David e CERÓN MUÑOZ, Hernán Darío e CATALANO, Fernando Martini. Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-3850. Acesso em: 04 nov. 2024.APA
Bravo Mosquera, P. D., Cerón Muñoz, H. D., & Catalano, F. M. (2019). Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-3850NLM
Bravo Mosquera PD, Cerón Muñoz HD, Catalano FM. Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system [Internet]. Proceedings. 2019 ;[citado 2024 nov. 04 ] Available from: https://doi.org/10.2514/6.2019-3850Vancouver
Bravo Mosquera PD, Cerón Muñoz HD, Catalano FM. Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system [Internet]. Proceedings. 2019 ;[citado 2024 nov. 04 ] Available from: https://doi.org/10.2514/6.2019-3850
