All Stories

  1. Characterization of a Vortex Wake Interaction Model

    Article • July 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Adson A De Paula

  2. Viscous and Non-Viscous Approaches for a Delta Wing Benchmark

    Article • July 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Adson A De Paula, Marcelo Hayashi

  3. A Non-Viscous Investigation of Mesh Refinement and Sweep Angle Effects on Combat Fighters

    Article • July 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Adson A De Paula

  4. The Influence of the Operational Altitude Variation on Flight Controller Design on Combat Aircraft Configuration

    Article • July 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Adson A De Paula, Éder Moura, LEONARDO NEPOMUCENO, Luiz Carlos Sandoval Góes

  5. The Wing Swept Angle Influence on Longitudinal Dynamic Stability in a Combat Aircraft Configuration

    Article • July 2024, American Institute of Aeronautics and Astronautics (AIAA)

    LEONARDO NEPOMUCENO, Luiz Carlos Sandoval Góes, Éder Moura, Dr Adson A De Paula

  6. Box wing longitudinal flight quality evaluation

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

    Dr Adson A De Paula

  7. Trijet and Twin-jet Aircraft Study For Optimal Aircraft Design

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

    Edgar Coelho Inouye, Dr Adson A De Paula

  8. Swept wing effects on Wavy Leading Edge Phenomena

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

    Dr Adson A De Paula

  9. The Wing Three-Dimensional Effects on Wavy Leading Edge Performance

    Article • June 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Adson A De Paula, Alejandro Arturo Rios Cruz, Thiago Thadeu da Silva Abrantes

  10. Optimization of High lift device system deployment for takeoff performance

    Article • June 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Adson A De Paula, Luiz Fernando Tibério Fernandez

  11. Aerodynamic Lateral-Directional Coefficients Modeling During Aircraft Design Phases

    Article • January 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Adson A De Paula, Mr Fabrício M Porto

  12. Matching of Aerodynamic databank with Flight test data - Latero-directional Dynamics

    Article • January 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Adson A De Paula, Mr Fabrício M Porto

  13. The Thickness Effect on Symmetrical Airfoil Flow Characteristics at low Reynolds number

    Article • January 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Adson A De Paula, Mr Fabrício M Porto

  14. Drag polar prediction methodologies during aircraft design phases

    Article • January 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Adson A De Paula, Mr Fabrício M Porto

  15. The Wavy Leading Edge Performance for a Very Thick Airfoil

    Article • January 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Adson A De Paula, Professor Julio R Meneghini

  16. Matching of Aerodynamic

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

    Dr Adson A De Paula, Mr Fabrício M Porto

  17. Aerodynamic Longitudinal Coefficients

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

    Dr Adson A De Paula, Mr Fabrício M Porto

  18. A Lean Product Development (LPD) approach on education and knowledge management in aircraft design

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

    Dr Adson A De Paula

  19. The Airfoil Thickness Effect on Wavy Leading Edge Performance

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

    Professor Julio R Meneghini, Dr Adson A De Paula

  20. Considerations about Wingtip Devices Design of Transport Airplane

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

    Dr Adson A De Paula

  21. Computational Aeroacoustics Analysis for Noise Minimization on the G550 Nose Landing Gear

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

    Professor Julio R Meneghini, Dr Adson A De Paula

  22. Performance of leading edge tubercles for a thin airfoil

    Article • January 2015, SWGE Sistemas

    Dr Adson A De Paula