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1
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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Artigo de Congresso 		Adicionar ao Meu Espaço

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)

2
The update process and characterization of the Sao Paulo University wind-tunnel for aeroacoustics testing
The update process and characterization of the Sao Paulo University wind-tunnel for aeroacoustics testing
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Artigo de Congresso 		Adicionar ao Meu Espaço

The update process and characterization of the Sao Paulo University wind-tunnel for aeroacoustics testing

Leandro Dantas Santana Fernando Martini Catalano; Marcello Augusto Faraco de Medeiros; Micael Carmo; International Congress of the Aeronautical Sciences - ICAS (27. : 2010 : Nice, France)

Proceedings Edinburgh, UK : Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2010

Edinburgh, UK Optimage Ltd/International Council of Aeronautical Sciences - ICAS 2010

Item não circula. Consulte sua biblioteca.(Acessar)

3
Acoustic control of laminar separation bubbles
Acoustic control of laminar separation bubbles
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Acoustic control of laminar separation bubbles

Luiz Guilherme Noujain Correa Ricardo Maiko Uehoka Entz; Renato Cosin; Fernando Martini Catalano; International Congress of the Aeronautical Sciences - ICAS (27. : 2010 : Nice, France)

Proceedings Edinburgh, UK : Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2010

Edinburgh, UK Optimage Ltd/International Council of Aeronautical Sciences - ICAS 2010

Item não circula. Consulte sua biblioteca.(Acessar)

4
An experimental study on wingtip devices for agricultural aircraft
An experimental study on wingtip devices for agricultural aircraft
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Artigo de Congresso 		Adicionar ao Meu Espaço

An experimental study on wingtip devices for agricultural aircraft

Rogerio Frauendorf de Faria Coimbra 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)

5
Wind tunnel testing of porous devices for the reduction of flap side-edge noise
Wind tunnel testing of porous devices for the reduction of flap side-edge noise
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Wind tunnel testing of porous devices for the reduction of flap side-edge noise

Fernando Martini Catalano Paulo Vanuchi; Luiz Guilherme Noujain Correa; 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)

6
Experimental and numerical study of two-element wing with gurney flap
Experimental and numerical study of two-element wing with gurney flap
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Artigo de Congresso 		Adicionar ao Meu Espaço

Experimental and numerical study of two-element wing with gurney flap

Fernando Martini Catalano Gerson Luiz Brand; International Congress of the Aeronautical Sciences - ICAS (25. : 2006 : Hamburg, Germany)

Proceedings Edinburgh, UK : Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2006

Edinburgh, UK Optimage Ltd/International Council of Aeronautical Sciences - ICAS 2006

Item não circula. Consulte sua biblioteca.(Acessar)

7
Wind tunnel wall boundary layer control for 2D high lift wing testing
Wind tunnel wall boundary layer control for 2D high lift wing testing
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Wind tunnel wall boundary layer control for 2D high lift wing testing

Fernando Martini Catalano Paulo Roberto Caixeta Junior; 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)

8
Experimental analysis of the confluent boundary layer between a flap and a main element with saw-toothed trailing edge
Experimental analysis of the confluent boundary layer between a flap and a main element with saw-toothed trailing edge
Material Type:
Artigo de Congresso 		Adicionar ao Meu Espaço

Experimental analysis of the confluent boundary layer between a flap and a main element with saw-toothed trailing edge

Rodrigo Cristian Lemes Fernando Martini Catalano; 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)

9
Passive, active, and adaptative systems for wing vortex drag reduction
Passive, active, and adaptative systems for wing vortex drag reduction
Material Type:
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Passive, active, and adaptative systems for wing vortex drag reduction

Hernán Darío Cerón Muñoz Fernando Martini Catalano; R. F Coimbra; International Congress of the Aeronautical Sciences - ICAS (26. : 2008 : Anchorage, Alaska, USA)

Proceedings Edinburgh, UK : Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2008

Edinburgh, UK Optimage Ltd/International Council of Aeronautical Sciences - ICAS 2008

Item não circula. Consulte sua biblioteca.(Acessar)

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