All Stories

  1. Aero-Propulso-Elastic Analysis of a Supersonic Transport

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

    Joseph W Connolly, Dr. Walter A Silva

  2. A Position on Current Stability and Control Prediction Capabilities and a Path Forward

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

    Dr. Michael A Niestroy, Dr. Walter A Silva

  3. Aeroelastic Indicial Response Reduced-Order Modeling for Flexible Flight Vehicles

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

    Dr. Walter A Silva

  4. Aeroelastic Indicial Response Reduced-Order Modeling for Flexible Flight Vehicles

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

    Dr. Walter A Silva

  5. Active Flutter Suppression Using Reduced Order Modeling for Transonic Aeroservoelastic Control Law Development

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

    Dr. Walter A Silva

  6. Reduced Order Modeling for Transonic Aeroservoelastic Control Law Development

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

    Dr. Walter A Silva

  7. Volterra Kernels Assessment via Time-Delay Neural Networks for Nonlinear Unsteady Aerodynamic Loading Identification

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

    Dr. Walter A Silva

  8. Computational Results for the KTH-NASA Wind-Tunnel Model Used for Acquisition of Transonic Nonlinear Aeroelastic Data

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

    Dr. Walter A Silva

  9. Identification and Analysis of Aeroelastic Systems Accounting for the Combined Effects of Aerodynamic and Structural Nonlinearities

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

    Dr. Walter A Silva, Hideaki Ogawa

  10. A Status Review of the Commercial Supersonic Technology (CST) Aeroservoelasticity (ASE) Project

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

    Dr. Walter A Silva

  11. Using FUN3D for Aeroelatic, Sonic Boom, and AeroPropulsoServoElastic (APSE) Analyses of a Supersonic Configuration

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

    Dr. Walter A Silva

  12. Towards an Aero-Propulso-Servo-Elasticity Analysis of a Commercial Supersonic Transport

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

    Joseph W Connolly, Dr. Walter A Silva

  13. Status of the KTH-NASA Wind-Tunnel Test for Acquisition of Transonic Nonlinear Aeroelastic Data

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

    Dr. Walter A Silva

  14. Ongoing Fixed Wing Research within the NASA Langley Aeroelasticity Branch

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

    Dr. Walter A Silva

  15. Computational Aeroelastic Analyses of a Low-Boom Supersonic Configuration

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

    Dr. Walter A Silva

  16. An Overview of the NASA High Speed ASE Project: Aeroelastic Analyses of a Low-Boom Supersonic Configuration

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

    James Florance, Dr. Walter A Silva

  17. Evaluation of Linear, Inviscid, Viscous, and Reduced-Order Modeling Aeroelastic Solutions of the AGARD 445.6 Wing Using Root Locus Analysis

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

    Dr. Walter A Silva

  18. A Summary of Revisions Applied to a Turbulence Response Analysis Method for Flexible Aircraft Configurations

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

    Dr. Walter A Silva

  19. The NASA High Speed ASE Project: Computational Analyses of a Low-Boom Supersonic Configuration

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

    Dr. Walter A Silva