All Stories

  1. Comparison of Computational and Experimental Ice Accretions of Large Swept Wings

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

    Gustavo Eidji C Fujiwara

  2. Method for Designing Hybrid Airfoils for Icing Wind-Tunnel Tests

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

    Gustavo Eidji C Fujiwara

  3. Method for Designing Three-Dimensional Swept Hybrid Wings for Icing Wind-Tunnel Tests

    Article • Journal of Aircraft, December 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Gustavo Eidji C Fujiwara

  4. Optimization of Variable-Camber Continuous Trailing-Edge Flap Configuration for Drag Reduction

    Article • Journal of Aircraft, November 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Gustavo Eidji C Fujiwara, Dr Nhan Nguyen

  5. Aerostructural Design Optimization of a Flexible Wing Aircraft with Continuous Morphing Trailing Edge

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

    Gustavo Eidji C Fujiwara

  6. 3D Computational Icing Method for Aircraft Conceptual Design

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

    Gustavo Eidji C Fujiwara

  7. Transonic and Viscous Potential Flow Method Applied to Flexible Wing Transport Aircraft

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

    Dr Nhan Nguyen, Gustavo Eidji C Fujiwara

  8. Aeroestructural Design Optimization of a Subsonic Wing with Continuous Morphing Trailing Edge

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

    Gustavo Eidji C Fujiwara, Dr Nhan Nguyen

  9. Computational and Experimental Ice Accretions of Large Swept Wings in the Icing Research Tunnel

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

    Gustavo Eidji C Fujiwara

  10. An Integral Boundary Layer Direct Method Applied to 2D Transonic Small-Disturbance Equations

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

    Gustavo Eidji C Fujiwara, Dr Nhan Nguyen

  11. Aerodynamic Modeling of Transonic Aircraft Using Vortex Lattice Coupled with Transonic Small Disturbance for Conceptual Design

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

    Gustavo Eidji C Fujiwara, Dr Nhan Nguyen

  12. Adaptive Aeroelastic Wing Shape Optimization for High-Lift Configurations

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

    Dr Nhan Nguyen, Gustavo Eidji C Fujiwara

  13. A Damage Assessment for Wind Turbine Blades from Heavy Atmospheric Particles

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

    Gustavo Eidji C Fujiwara

  14. 3D Swept Hybrid Wing Design Method for Icing Wind Tunnel Tests

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

    Gustavo Eidji C Fujiwara

  15. Large-Scale Swept-Wing Icing Simulations in the NASA Glenn Icing Research Tunnel Using LEWICE3D

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

    Gustavo Eidji C Fujiwara

  16. Design of a Human-Powered Aircraft Applying Multidisciplinary Optimization Method

    Article • September 2013, SAE International

    Gustavo Eidji C Fujiwara

  17. A Hybrid Airfoil Design Method for Icing Wind Tunnel Tests

    Article • June 2013, American Institute of Aeronautics and Astronautics (AIAA)

    Gustavo Eidji C Fujiwara