Potential propulsive and aerodynamic benefits of a new aircraft concept: a low-speed experimental study (2023)
- Authors:
- USP affiliated authors: MUÑOZ, HERNAN DARIO CERON - EESC ; CATALANO, FERNANDO MARTINI - EESC ; MOSQUERA, PEDRO DAVID BRAVO - EESC
- Unidade: EESC
- DOI: 10.3390/aerospace10070651
- Subjects: AERODINÂMICA DE AERONAVES; TÚNEIS DE VENTO; ENGENHARIA AERONÁUTICA
- Agências de fomento:
- Language: Inglês
- Imprenta:
- Publisher: MDPI AG
- Publisher place: Basel, Switzerland
- Date published: 2023
- Source:
- Este periódico é de acesso aberto
- Este artigo NÃO é de acesso aberto
-
ABNT
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: 17 fev. 2026. -
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/aerospace10070651 -
NLM
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 2026 fev. 17 ] Available from: https://doi.org/10.3390/aerospace10070651 -
Vancouver
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 2026 fev. 17 ] Available from: https://doi.org/10.3390/aerospace10070651 - Design, aerodynamic analysis and optimization of a next‑generation commercial airliner
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Informações sobre o DOI: 10.3390/aerospace10070651 (Fonte: oaDOI API)
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