Pedro Jose Boschetti Castro
Pedro Jose Boschetti Castro
Associate Professor, Universidad Simón Bolívar, Venezuela
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Design of an unmanned aerial vehicle for ecological conservation
EM Cárdenas, PJ Boschetti, A Amerio, CD Velásquez
Infotech@Aerospace, 2005
272005
Stability and Performance of a Light Unmanned Airplane in Ground Effect
PJ Boschetti, EM Cárdenas, A Amerio, A Arévalo
48th AIAA Aerospace Sciences Meeting and Exhibit, 2010
262010
Diseño de un Avión No Tripulado de Conservación Ecológica
P Boschetti, E Cárdenas
Theses, Department of Aeronautical Engineering, Universidad Nacional …, 2003
142003
Increasing the Lift-Drag Ratio of an Unmanned Aerial VehicleUusing Local Twist
PJ Boschetti, EM Cárdenas, A Amerio
Journal of aircraft 45 (1), 10-15, 2008
132008
Stability and Flying Qualities of an Unmanned Airplane Using the Vortex-Lattice Method
EM Cárdenas, PJ Boschetti, A Amerio
Journal of aircraft 46 (4), 1461-1465, 2009
122009
Ground effect on the longitudinal stability of an unmanned airplane
P Boschetti, E Cardenas
50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and …, 2012
102012
Reducción de Resistencia Aerodinámica en el Avión No Tripulada de Conservación Ecológica
P Boschetti
Universidad Simón Bolívar. Decanato de estudios de Postgrado. Maestría en …, 2006
102006
Drag Clean-Up Process of Unmanned Airplane for Ecological Conservation
PJ Boschetti, EM Cárdenas, A Amerio
Aerotecnica, Missili e Spazio 85 (2), 53-62, 2006
82006
Aerodynamic Optimization of an UAV Design
PJ Boschetti, EM Cárdenas, A Amerio
AIAA 5th Aviation Technology Integration and Operation, 2005
82005
Design of Control Systems to Hold Altitude and Heading in Severe Atmospheric Disturbances for an Unmanned Airplane
EM Cárdenas, PJ Boschetti, MR Celi
50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and …, 2012
62012
Experimental Aerodynamic Study of UAV Wind Tunnel Model for Low Reynolds Number
PJ Boschetti, M Cárdenas Elsa, NR García
22nd Applied Aerodynamics Conference and Exhibit, 1-7, 2004
52004
Design of a Landing Control System which considers Dynamic Ground Effect for an Unmanned Airplane
PJ González, PJ Boschetti, EM Cárdenas, M Rodríguez
1st WSEAS International Conference on Aeronautical and Mechanical Engineering, 2013
4*2013
Induced Drag Reduction of an Airplane using Local Twist, Panel Method Verification
PJ Boschetti, EM Cárdenas, A Amerio
50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and …, 2012
32012
Evaluation of the Flying Qualities of a Half-Scale Unmanned Airplane via Flight Simulation
PJ González, PJ Boschetti, EM Cárdenas, A Amerio
48th AIAA Aerospace Sciences Meeting and Exhibit, 2010
32010
Stability of an Unmanned Airplane Using a Low-Order Panel Method
P Boschetti, E Cárdenas, A Amerio
AIAA Atmospheric Flight Mechanics Conference, 2010
32010
Dynamic Ground Effect on the Aerodynamic Coefficients of a Wing using a Panel Method
PJ Boschetti, G Quijada, EM Cárdenas
AIAA Atmospheric Flight Mechanics Conference, 3104, 2016
22016
Static-Stability Analysis of an Unmanned Airplane as a Flexible-Body
OE González, PJ Boschetti, EM Cárdenas, A Amerio
AIAA Atmospheric Flight Mechanics Conference, 2010
22010
Aerodynamic Performance as a Function of Local Twist in an Unmanned Airplane
PJ Boschetti, A Amerio, EM Cárdenas
47th AIAA Aerospace Sciences Meeting and Exhibit, 2009
22009
Evaluación de la Estabilidad Estática de un Avión No Tripulado Empleando el Método Vortex Lattice
E Cárdenas, P Boschetti, A Amerio
IX Congreso Internacional de Métodos Numéricos Ingeniería y Ciencias, 2008
22008
Simulación Numérica de la Sustentación en el Ala de un Avión No Tripulado
P Boschetti, E Cárdenas, A Amerio
VIII Congreso Internacional de Métodos Numéricos en Ingeniería y Ciencias …, 2006
2*2006
El sistema no puede realizar la operación en estos momentos. Inténtalo de nuevo más tarde.
Artículos 1–20