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 é de acesso aberto
- URL de acesso aberto
- Cor do Acesso Aberto: gold
- Licença: cc-by
-
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: 02 out. 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/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 2024 out. 02 ] 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 2024 out. 02 ] Available from: https://doi.org/10.3390/aerospace10070651 - Conceptual design and CFD analysis of a new prototype of agricultural aircraft
- Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system
- Design, aerodynamic analysis and optimization of a next‑generation commercial airliner
- Experimental analyses of droop, wingtips and fences on a BWB model
- Unconventional aircraft for civil aviation
- Design and manufacture of a solar-powered unmanned aerial vehicle for civilian surveillance missions
- Integration assessment of conceptual design and intake aerodynamics of a non-conventional air-to-ground fighter aircraf
- Conceptual and aerodynamic design of a UAV for superficial volcano monitoring
- Design and performance assessment of an inverted rectangular dorsal intake for military aviation
- Experimental analysis of aerodynamics characteristics of adaptative multi-winglets
Informações sobre o DOI: 10.3390/aerospace10070651 (Fonte: oaDOI API)
Download do texto completo
Tipo | Nome | Link | |
---|---|---|---|
aerospace-10-00651 (2)_co... | Direct link |
How to cite
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas