Trailing edge treatment to enhance high lift system performance (2012)
- Authors:
- USP affiliated authors: CATALANO, FERNANDO MARTINI - EESC ; MUÑOZ, HERNAN DARIO CERON - EESC ; GRECO JUNIOR, PAULO CELSO - EESC
- Unidade: EESC
- Subjects: ASAS DE AERONAVES; AEROFÓLIOS; ENGENHARIA AERONÁUTICA
- Language: Inglês
- Imprenta:
- Publisher: Optimage Ltd/International Council of Aeronautical Sciences - ICAS
- Publisher place: Edinburgh, UK
- Date published: 2012
- Source:
- Título: Proceedings
- Conference titles: International Congress of the Aeronautical Sciences - ICAS
-
ABNT
CATALANO, Fernando Martini e CERÓN MUÑOZ, Hernán Darío e GRECO JÚNIOR, Paulo Celso. Trailing edge treatment to enhance high lift system performance. 2012, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2012. . Acesso em: 01 jan. 2026. -
APA
Catalano, F. M., Cerón Muñoz, H. D., & Greco Júnior, P. C. (2012). Trailing edge treatment to enhance high lift system performance. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS. -
NLM
Catalano FM, Cerón Muñoz HD, Greco Júnior PC. Trailing edge treatment to enhance high lift system performance. Proceedings. 2012 ;[citado 2026 jan. 01 ] -
Vancouver
Catalano FM, Cerón Muñoz HD, Greco Júnior PC. Trailing edge treatment to enhance high lift system performance. Proceedings. 2012 ;[citado 2026 jan. 01 ] - Pressure measurements in oscillatory NACA0012 airfoil: experimental and computational results
- Analytical and numerical design of a mixed-compression air intake for a supersonic fighter aircraft
- Experimental analysis of aerodynamics characteristics of adaptative multi-winglets
- Análisis computacional del control de la capa límite, en perfiles para uso en turbinas eólicas
- Análisis computacional de las características aerodinámicas de un vant en configuración "box-wing"
- Analysis of geometric and flying characteristics of Santos Dumont's 14-BIS
- Viscous and wage drag optimization for a transport aircraft mission adaptive wing
- Aeordynamic databased of a subscale demonstrator
- Aerodynamic interference of power-plant system on a blended wing body
- Estudo da influência aerodinâmica de dispositivos de ponta de asa em uma aeronave do tipo "blended wing body"
How to cite
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
