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Pedro Jose Boschetti Castro
Pedro Jose Boschetti Castro
Associate Professor, Universidad Simón Bolívar, Venezuela
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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
312010
Design of an unmanned aerial vehicle for ecological conservation
EM Cárdenas, PJ Boschetti, A Amerio, CD Velásquez
Infotech@Aerospace, 2005
312005
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
172009
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
152012
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
152008
Diseño de un Avión No Tripulado de Conservación Ecológica
P Boschetti, E Cárdenas
Theses, Department of Aeronautical Engineering, Universidad Nacional …, 2003
142003
Reducción de resistencia aerodinámica en el avión no tripulado de conservación ecológica
P Boschetti
Universidad Simón Bolívar. Decanato de estudios de Postgrado. Maestría en …, 2006
112006
Aerodynamic Optimization of an UAV Design
PJ Boschetti, EM Cárdenas, A Amerio
AIAA 5th Aviation Technology Integration and Operation, 2005
112005
Drag Clean-Up Process of the Unmanned Airplane for Ecological Conservation
PJ Boschetti, EM Cárdenas, A Amerio
Aerotecnica, Missili e Spazio 85 (2), 53-62, 2006
102006
Nonlinear aerodynamic model for wings in dynamic ground effect
PJ Boschetti, EM Cárdenas, PJ González, A Merkl
Journal of Aircraft 57 (6), 1234-1241, 2020
72020
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
72016
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
72013
Dynamic Ground Effect on the Aerodynamic Coefficients Using a Panel Method
PJ Boschetti, GM Quijada, EM Cárdenas
Journal of Aircraft 54 (2), 838-844, 2017
62017
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
62012
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
62004
Lattice Boltzmann simulation of swelling behavior of cylindrical IPN hydrogel tablets
PJ Boschetti, O Pelliccioni, MA Sabino, N Vera, MF Pappaterra
Fluid Phase Equilibria 508, 112449, 2020
52020
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
52010
Lattice Boltzmann simulation of swelling of an implant for microtia manufactured with IPN hydrogel
PJ Boschetti, O Pelliccioni, K Da Costa, MA Sabino
Computer Methods in Biomechanics and Biomedical Engineering 23, 2020
42020
Swelling behavior of IPN and copolymer hydrogels by Lattice Boltzmann Method
PJ Boschetti, OJ Pelliccioni, M Sabino, N Vera, A Ontiveros, ...
AIAA Scitech 2020 Forum, 2234, 2020
42020
El sistema no puede realizar la operación en estos momentos. Inténtalo de nuevo más tarde.
Artículos 1–20