Fernando Martini Catalano
Fernando Martini Catalano
Professor of aerodynamics University of Sao Paulo
Verified email at sc.usp.br
Cited by
Cited by
On the effects of an installed propeller slipstream on wing aerodynamic characteristics
FM Catalano
Acta Polytechnica 44 (3), 2004
Conceptual design and CFD analysis of a new prototype of agricultural aircraft
PD Bravo-Mosquera, HD Cerón-Muñoz, G Díaz-Vázquez, FM Catalano
Aerospace Science and Technology 80, 156-176, 2018
Experimental investigation of wing-tip devices on the reduction of induced drag
HD Céron-Muñoz, R Cosin, RFF Coimbra, LGN Correa, FM Catalano
Journal of Aircraft 50 (2), 441-449, 2013
Drag optimization for transport aircraft Mission Adaptive Wing
AL Martins, FM Catalano
Journal of the Brazilian Society of Mechanical Sciences and Engineering 25 …, 2003
The update of an aerodynamic wind-tunnel for aeroacoustics testing
LD Santana, M Carmo, FM Catalano, MAF Medeiros
Journal of Aerospace Technology and Management 6, 111-118, 2014
Experimental analysis of the aerodynamic characteristics adaptive of multi-winglets
HD Cerón-Muñoz, FM Catalano
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2006
Experimental analysis of aerodynamics characteristics of adaptive multi-winglets
F Catalano, H Ceron-Muñoz
43rd AIAA Aerospace Sciences Meeting and Exhibit, 1231, 2005
The new closed circuit wind tunnel of the aircraft laboratory of University of São Paulo
F Catalano
16th Brazilian Congress of Mechanical Engineering 6, 306-312, 2001
Viscous drag optimization for a transport aircraft mission adaptive wing
AL Martins, FM Catalano
Prog. 21st ICAS Congress, Melbourne, Australia, A98-31499, 1998
Aerodynamic analysis of multi-winglets for low speed aircraft
R Cosin, FM Catalano, LGN Correa, RMU Entz
27th International congress of the aeronautical sciences, 2010
The new closed circuit wind tunnel of the aircraft laboratory of university of sao paulo, brazil
F Catalano
24TH International Congress of the Aeronautical Sciencies ICAS, 2004
Fuel efficiency improvement on a business jet using a camber morphing winglet concept
JP Eguea, GPG da Silva, FM Catalano
Aerospace Science and Technology 96, 105542, 2020
Integration assessment of conceptual design and intake aerodynamics of a non-conventional air-to-ground fighter aircraft
PD Bravo-Mosquera, AM Abdalla, HD Cerón-Muñoz, FM Catalano
Aerospace Science and Technology 86, 497-519, 2019
Projeto, construção e calibração em túnel aerodinâmico de circuito aberto tipo NPL de seção transversal hexagonal
FM Catalano
USP: São Carlos, 1988
Slat aerodynamic noise reduction using dielectric barrier discharge plasma actuators
GPG da Silva, JP Eguea, JAG Croce, FM Catalano
Aerospace Science and Technology 97, 105642, 2020
Parametric analysis of the influence of slat geometry on acoustic noise
L Botero, LT Lima Pereira, D Acevedo, F Catalano, DC Reis, EL Coelho
2018 AIAA/CEAS Aeroacoustics Conference, 3593, 2018
Predicting turbulent decorrelation in acoustic phased arrays
L Pires, R Dougherty, S Gerges, F Catalano
50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and …, 2012
Novel hybrid electric motor glider-quadrotor MAV for in-flight/V-STOL launching
RCB Sampaio, AC Hernandes, M Becker, FM Catalano, F Zanini, ...
2014 IEEE Aerospace Conference, 1-12, 2014
The update process and characterization of the Sao Paulo University wind-tunnel for aeroacoustics testing
L Santana, FM Catalano, MAF Medeiros, M Carmo
27th ICAS, Nice France, 2010
Aerodynamic optimization study of a mission adaptive wing for transport aircraft
A Martinz, F Catalano, A Martinz, F Catalano
15th Applied Aerodynamics Conference, 2272, 1996
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