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1
Numerical and experimental analysis of the effect of a pusher propeller on a wing
Numerical and experimental analysis of the effect of a pusher propeller on a wing
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Numerical and experimental analysis of the effect of a pusher propeller on a wing

Fernando Martini Catalano M G Maunsell; Congress of the International Council of the Aeronautical Sciences (20. 1996 Sorrento)

Proceedings Sorrento : Aiaa/Icas, 1996

Sorrento Aiaa/Icas 1996

Localização: EESC - Esc. Engenharia de São Carlos    (PROD-001628 )(Acessar)

2
Viscous drag optimization for a transport aircraft mission adaptive wing. [CD-ROM]
Viscous drag optimization for a transport aircraft mission adaptive wing. [CD-ROM]
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Viscous drag optimization for a transport aircraft mission adaptive wing. [CD-ROM]

André Luiz Martins Fernando Martini Catalano; Congress of the International Council of the Aeronautical Sciences (21. 1998 Melbourne)

Proceedings Melbourne : ICAS/AIAA, 1998

Melbourne ICAS/AIAA 1998

Item não circula. Consulte sua biblioteca.(Acessar)

3
Theoretical study of a mission adaptive wing
Theoretical study of a mission adaptive wing
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Theoretical study of a mission adaptive wing

A L Martins Fernando Martini Catalano; Congress of the International Council of the Aeronautical Sciences (20. 1996 Sorrento)

Proceedings Sorrento : Aiaa/Icas, 1996

Sorrento Aiaa/Icas 1996

Item não circula. Consulte sua biblioteca.(Acessar)

4
On the effects of a installed propeller slipstream on a wing boundary layer
On the effects of a installed propeller slipstream on a wing boundary layer
Material Type:
Artigo de Congresso 		Adicionar ao Meu Espaço

On the effects of a installed propeller slipstream on a wing boundary layer

Fernando Martini Catalano International Congress of the Aeronautical Sciences - ICAS (22. : 2000 : Harrogate, UK)

Proceedings Edinburgh, UK : ICAS, 2000

Edinburgh, UK ICAS 2000

Localização: EESC - Esc. Engenharia de São Carlos    (PROD-023761 )(Acessar)

5
The new closed circuit wind tunnel of the aircraft laboratory of University of São Paulo, Brazil
The new closed circuit wind tunnel of the aircraft laboratory of University of São Paulo, Brazil
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The new closed circuit wind tunnel of the aircraft laboratory of University of São Paulo, Brazil

Fernando Martini Catalano International Congress of the Aeronautical Sciences - ICAS (24. : 2004 : Yokohama, Japan)

Proceedings Edinburgh, UK : ICAS, 2004

Edinburgh, UK ICAS 2004

Localização: EESC - Esc. Engenharia de São Carlos    (PROD-023758 )(Acessar)

6
Experimental analysis of the aerodynamics of porous flap side-edge
Experimental analysis of the aerodynamics of porous flap side-edge
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Experimental analysis of the aerodynamics of porous flap side-edge

F. P. Moraleda Fernando Martini Catalano; International Congress of the Aeronautical Sciences - ICAS (29. : 2014 : St. Petersburg, Russia)

Proceedings Edinburgh, UK : Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2014

Edinburgh, UK Optimage Ltd/International Council of Aeronautical Sciences - ICAS 2014

Item não circula. Consulte sua biblioteca.(Acessar)

7
Conceptual design and optimization of a high aspect ratio UAV wing made of composite material
Conceptual design and optimization of a high aspect ratio UAV wing made of composite material
Material Type:
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Conceptual design and optimization of a high aspect ratio UAV wing made of composite material

K Widmaier Fernando Martini Catalano; International Congress of the Aeronautical Sciences - ICAS (22. : 2000 : Harrogate, UK)

Proceedings Edinburgh, UK : Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2000

Edinburgh, UK Optimage Ltd/International Council of Aeronautical Sciences - ICAS 2000

Item não circula. Consulte sua biblioteca.(Acessar)

8
Computational investigation of icing contamination on airfoil
Computational investigation of icing contamination on airfoil
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Computational investigation of icing contamination on airfoil

Thaís Bortholin Fernando Martini Catalano; International Congress of the Aeronautical Sciences - ICAS (28. : 2012 : Brisbane, Australia)

Proceedings Edinburgh, UK : Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2012

Edinburgh, UK Optimage Ltd/International Council of Aeronautical Sciences - ICAS 2012

Item não circula. Consulte sua biblioteca.(Acessar)

9
Analysis of geometric and flying characteristics of Santos Dumont's 14-BIS
Analysis of geometric and flying characteristics of Santos Dumont's 14-BIS
Material Type:
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Analysis of geometric and flying characteristics of Santos Dumont's 14-BIS

Paulo Celso Greco Júnior Fernando Martini Catalano; Brazilian Congress of Thermal Sciences and Engineering - ENCIT (11. : 2006 : Curitiba, PR)

Proceedings [Curitiba, PR] : ABCM, 2006

Curitiba, PR ABCM 2006

Item não circula. Consulte sua biblioteca.(Acessar)

10
Experimental analysis of aerodynamics characteristics of adaptative multi-winglets
Experimental analysis of aerodynamics characteristics of adaptative multi-winglets
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Artigo de Congresso 		Adicionar ao Meu Espaço

Experimental analysis of aerodynamics characteristics of adaptative multi-winglets

Fernando Martini Catalano Hernán Darío Cerón Muñoz; International Congress of the Aeronautical Sciences - ICAS (24. : 2004 : Yokohama, Japan)

Proceedings Edinburgh, UK : Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2004

Edinburgh, UK Optimage Ltd/International Council of Aeronautical Sciences - ICAS 2004

Item não circula. Consulte sua biblioteca.(Acessar)

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