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  1. Nonlinear Aerodynamic Model in Dynamic Ground Effect at High Angles of Attack

    Article • Journal of Aircraft, June 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Prof Pedro J Boschetti

  2. Nonlinear Aerodynamic Model in Dynamic Ground Effect at High Angles of Attack

    Article • January 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Prof Pedro J Boschetti

  3. Unsteady Aerodynamic Analysis of a Light Unmanned Airplane in Ground Effect

    Article • January 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Prof Pedro J Boschetti

  4. Lattice Boltzmann method simulations of swelling of cuboid-shaped IPN hydrogel tablets with experimental validation

    Article • Heat and Mass Transfer, October 2021, Springer Science + Business Media

    Prof Pedro J Boschetti

  5. Nonlinear Aerodynamic Model for Wings in Dynamic Ground Effect

    Article • Journal of Aircraft, June 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Prof Pedro J Boschetti, Pedro Gonzalez, Alejandro Merkl

  6. Lattice Boltzmann simulation of swelling of an implant for microtia manufactured with IPN hydrogel

    Article • Computer Methods in Biomechanics & Biomedical Engineering, March 2020, Taylor & Francis

    Prof Pedro J Boschetti

  7. Lattice Boltzmann simulation of swelling behavior of cylindrical IPN hydrogel tablets

    Article • Fluid Phase Equilibria, March 2020, Elsevier

    Prof Pedro J Boschetti

  8. Swelling Behavior of IPN and Copolymer Hydrogels by Lattice Boltzmann Method

    Article • January 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Prof Pedro J Boschetti

  9. Dynamic Stability and Flying Qualities of an Unmanned Airplane as a Flexible Body

    Article • January 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Prof Pedro J Boschetti

  10. Integrated Structural, Flight Dynamics and Aeroelastic Analysis of the ANCE X-3d as a Flexible Body

    Article • January 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Prof Pedro J Boschetti, Pedro Gonzalez, Luis Hernandez

  11. Dependence of the Flight-path on the Aerodynamic Characteristics of Rectangular Wings due to Dynamic Ground Effect

    Article • January 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Prof Pedro J Boschetti, Alejandro Merkl

  12. Nonlinear Models for Representing Aerodynamic Coefficients of a Wing in Ground Effect

    Article • January 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Prof Pedro J Boschetti

  13. Contribution of a Running Propeller in the Longitudinal Stability of an Airplane by an Analytical-Empirical Analysis

    Article • January 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Isaac Taboada, Prof Pedro J Boschetti

  14. Dynamic Ground Effect on the Aerodynamic Coefficients Using a Panel Method

    Article • Journal of Aircraft, October 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Prof Pedro J Boschetti

  15. Influence of Piston Propeller-driven engine Model into the Design of Cruise Autopilot

    Article • June 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Prof Pedro J Boschetti

  16. Dynamic Ground Effect on the Aerodynamic Coefficients of a Wing using a Panel Method

    Article • June 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Prof Pedro J Boschetti

  17. Program to Calculate the Performance of Airplanes Driven by a Fixed-Pitch Propeller

    Article • January 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Pedro Gonzalez, Prof Pedro J Boschetti

  18. Linear Computational Fluid Dynamic Analysis of Dynamic Ground Effect of a Wing in Sink and Flare Maneuvers

    Article • January 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Prof Pedro J Boschetti

  19. Dynamic Ground Effect on the Longitudinal Stability of Airplanes during the Landing

    Article • January 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Pedro Gonzalez, Prof Pedro J Boschetti

  20. Evaluation of the Flying Qualities of a Light Unmanned Airplane via Flight Simulation

    Article • January 2012, American Institute of Aeronautics and Astronautics (AIAA)

    Pedro Gonzalez, Prof Pedro J Boschetti

  21. Ground Effect on the Longitudinal Stability of an Unmanned Airplane

    Article • January 2012, American Institute of Aeronautics and Astronautics (AIAA)

    Prof Pedro J Boschetti

  22. Induced Drag Reduction of an Airplane Using Local Twist, Panel Method Verification

    Article • January 2012, American Institute of Aeronautics and Astronautics (AIAA)

    Prof Pedro J Boschetti

  23. Design of Control Systems to Hold Altitude and Heading in Severe Atmospheric Disturbances for an Unmanned Airplane

    Article • January 2012, American Institute of Aeronautics and Astronautics (AIAA)

    Prof Pedro J Boschetti

  24. Stability of an Unmanned Airplane Using a Low-Order Panel Method

    Article • August 2010, American Institute of Aeronautics and Astronautics (AIAA)

    Prof Pedro J Boschetti

  25. Static-Stability Analysis of an Unmanned Airplane as a Flexible-Body

    Article • August 2010, American Institute of Aeronautics and Astronautics (AIAA)

    Prof Pedro J Boschetti

  26. Evaluation of the Flying Qualities of a Half-Scale Unmanned Airplane via Flight Simulation

    Article • January 2010, American Institute of Aeronautics and Astronautics (AIAA)

    Pedro Gonzalez, Prof Pedro J Boschetti

  27. Stability and Performance of a Light Unmanned Airplane in Ground Effect

    Article • January 2010, American Institute of Aeronautics and Astronautics (AIAA)

    Prof Pedro J Boschetti

  28. Stability and Flying Qualities of an Unmanned Airplane Using the Vortex-Lattice Method

    Article • Journal of Aircraft, July 2009, American Institute of Aeronautics and Astronautics (AIAA)

    Prof Pedro J Boschetti

  29. Aerodynamic Analysis of the Unmanned Aerial Vehicle for Ecological Conservation

    Article • January 2009, American Institute of Aeronautics and Astronautics (AIAA)

    Prof Pedro J Boschetti

  30. Aerodynamic Performance as a Function of Local Twist in an Unmanned Airplane

    Article • January 2009, American Institute of Aeronautics and Astronautics (AIAA)

    Prof Pedro J Boschetti

  31. Stability and Flying Qualities of an Unmanned Airplane using Vortex Lattice Method

    Article • January 2009, American Institute of Aeronautics and Astronautics (AIAA)

    Prof Pedro J Boschetti

  32. Increasing the Lift-Drag Ratio of an Unmanned Aerial VehicleUusing Local Twist

    Article • Journal of Aircraft, January 2008, American Institute of Aeronautics and Astronautics (AIAA)

    Prof Pedro J Boschetti

  33. Increasing Lift-Drag Ratio of an Unmanned Aerial Vehicle using Local Twist

    Article • June 2007, American Institute of Aeronautics and Astronautics (AIAA)

    Prof Pedro J Boschetti

  34. Design of an Unmanned Aerial Vehicle for Ecological Conservation

    Article • September 2005, American Institute of Aeronautics and Astronautics (AIAA)

    Prof Pedro J Boschetti

  35. Aerodynamic Optimization of an UAV Design

    Article • September 2005, American Institute of Aeronautics and Astronautics (AIAA)

    Prof Pedro J Boschetti

  36. Experimental Aerodynamic Study of UAV Wind Tunnel Model for Low Reynolds Number

    Article • August 2004, American Institute of Aeronautics and Astronautics (AIAA)

    Prof Pedro J Boschetti