BRAZILIAN AVIATION HISTORY: THE UNIVERSITY OF SÃO PAULO CASE
MULTI-DISCIPLINARY DESIGN OPTIMIZATION OF A BLENDED WINGLET
ICAS2016_0003: LOW REYNOLDS PROPELLER META-MODEL FOR MULTIDICIPLYNARY OPTIMIZATION
ICAS2014_0606: EXPERIMENTAL ANALYSIS OF THE AERODYNAMICS OF POROUS FLAP SIDE-EDGE
INFLUENCE OF GULL WING ON LONGITUDINAL AND LATERAL-DIRECTIONAL COEFFICIENTS OF AN AIRPLANE
Experimental analysis of the aerodynamic characteristics adaptive of multi-winglets
Numerical and Experimental Analysis of the Effect of a Pusher Propeller on a Wing
Drag Optimization for Transport Aircraft Mission Adaptive Wing
DESIGN AND PERFORMANCE ASSESSMENT OF AN INVERTED RECTANGULAR DORSAL INTAKE FOR MILITARY AVIATION
Numerical and Experimental Analysis of the Effect of a Pusher Propeller on a Wing and Body
THE NEW CLOSED CIRCUIT WIND TUNNEL OF THE AIRCRAFT LABORATORY OF UNIV. OF SAO PAULO
ICAS2016_0397: CONCEPTUAL AND AERODYNAMIC DESIGN OF A UAV FOR SUPERFICIAL VOLCANO MONITORING
ICAS2014_0933: AERODYNAMIC INTERFERENCE OF WINGTIP AND WING DEVICES ON BWB MODEL
EXPERIMENTAL AND COMPUTATIONAL ANALYSIS OF A UAV FOR SUPERFICIAL VOLCANO SURVEILLANCE
EXPERIMENTAL ANALYSIS OF AERODYNAMICS CHARACTERISTICS OF ADAPTIVE MULTI-WINGLETS