Experimental analyses of droop, wingtips and fences on a BWB model (2016)
- Authors:
- USP affiliated authors: MUÑOZ, HERNAN DARIO CERON - EESC ; CATALANO, FERNANDO MARTINI - EESC ; IZQUIERDO, DAVID ORLANDO DIAZ - EESC ; MOSQUERA, PEDRO DAVID BRAVO - EESC
- Unidade: EESC
- Subjects: ASAS DE AERONAVES; AERODINÂMICA DE AERONAVES; ENGENHARIA AERONÁUTICA
- Language: Inglês
- Imprenta:
- Publisher: Optimage Ltd/International Council of Aeronautical Sciences - ICAS
- Publisher place: Edinburgh, UK
- Date published: 2016
- Source:
- Título do periódico: Proceedings
- Conference titles: International Congress of the Aeronautical Sciences - ICAS
-
ABNT
CERÓN MUÑOZ, Hernán Darío et al. Experimental analyses of droop, wingtips and fences on a BWB model. 2016, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2016. . Acesso em: 19 abr. 2024. -
APA
Cerón Muñoz, H. D., Diaz Izquierdo, D. O., Bravo Mosquera, P. D., & Catalano, F. M. (2016). Experimental analyses of droop, wingtips and fences on a BWB model. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS. -
NLM
Cerón Muñoz HD, Diaz Izquierdo DO, Bravo Mosquera PD, Catalano FM. Experimental analyses of droop, wingtips and fences on a BWB model. Proceedings. 2016 ;[citado 2024 abr. 19 ] -
Vancouver
Cerón Muñoz HD, Diaz Izquierdo DO, Bravo Mosquera PD, Catalano FM. Experimental analyses of droop, wingtips and fences on a BWB model. Proceedings. 2016 ;[citado 2024 abr. 19 ] - 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
- Potential propulsive and aerodynamic benefits of a new aircraft concept: a low-speed experimental study
- Design, aerodynamic analysis and optimization of a next‑generation commercial airliner
- Aerodynamic interference of wingtip and wing devices on BWB model
- Unconventional aircraft for civil aviation
- Design and manufacture of a solar-powered unmanned aerial vehicle for civilian surveillance missions
- Conceptual and aerodynamic design of a UAV for superficial volcano monitoring
- Integration assessment of conceptual design and intake aerodynamics of a non-conventional air-to-ground fighter aircraf
- Experimental analysis of aerodynamics characteristics of adaptative multi-winglets
How to cite
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas