All Stories

  1. Kestrel Results at Liftoff Conditions for a Space Launch System Configuration in Proximity to the Launch Tower

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

    Farhad Ghaffari, Nalin Ratnayake

  2. Computational Fluid Dynamics Methods Used in the Development of the Space Launch System Liftoff and Transition Lineloads Databases

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

    Nalin Ratnayake, Farhad Ghaffari

  3. Kestrel Results at Liftoff Conditions for a Space Launch System Configuration in Proximity to the Launch Tower

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

    Farhad Ghaffari, Nalin Ratnayake

  4. Selection of Computational Fluid Dynamics Tools Used in Development of the Space Launch System Liftoff and Transition Lineloads Databases

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

    Farhad Ghaffari, Nalin Ratnayake

  5. Results from DES Simulations of an SLS Variant at Liftoff Conditions with Comparison to Experiment

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

    Farhad Ghaffari

  6. Error Estimates of the Ares I Computed Turbulent Ascent Longitudinal Aerodynamic Analysis

    Article • Journal of Spacecraft and Rockets, July 2012, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Khaled S Abdol-Hamid, Farhad Ghaffari

  7. Ares I Vehicle Computed Turbulent Ascent Aerodynamic Data Development and Analysis

    Article • Journal of Spacecraft and Rockets, July 2012, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Khaled S Abdol-Hamid, Farhad Ghaffari

  8. Ares I Vehicle Computed Turbulent Ascent Aerodynamic Data Development and Analysis

    Article • Journal of Spacecraft and Rockets, July 2012, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Khaled S Abdol-Hamid, Farhad Ghaffari

  9. Error Estimates of the Ares I Computed Turbulent Ascent Longitudinal Aerodynamic Analysis

    Article • Journal of Spacecraft and Rockets, July 2012, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Khaled S Abdol-Hamid, Farhad Ghaffari

  10. Error Estimate of the Ares I Vehicle Longitudinal Aerodynamic Characteristics Based on Turbulent Navier-Stokes Analysis

    Article • June 2011, American Institute of Aeronautics and Astronautics (AIAA)

    Dr Khaled S Abdol-Hamid, Farhad Ghaffari

  11. On the vortical-flow-prediction capability of an unstructured-grid Euler solver

    Article • January 1994, American Institute of Aeronautics and Astronautics (AIAA)

    Farhad Ghaffari

  12. Multiblock Navier-Stokes solutions about the F/A-18 wing-LEX-fuselage configuration

    Article • Journal of Aircraft, May 1993, American Institute of Aeronautics and Astronautics (AIAA)

    Farhad Ghaffari

  13. Navier-Stokes solutions about the F/A-18 wing-LEX-fuselage configuration with multi-block structured grids

    Article • September 1991, American Institute of Aeronautics and Astronautics (AIAA)

    Farhad Ghaffari

  14. Application of a patched-grid algorithm to the F/A-18 forebody-leading-edge extension configuration

    Article • Journal of Aircraft, September 1990, American Institute of Aeronautics and Astronautics (AIAA)

    Farhad Ghaffari

  15. Analytical method for the ditching analysis of an airborne vehicle

    Article • Journal of Aircraft, April 1990, American Institute of Aeronautics and Astronautics (AIAA)

    Farhad Ghaffari

  16. Transonic Navier-Stokes solutions about a complex high-speed accelerator configuration

    Article • January 1990, American Institute of Aeronautics and Astronautics (AIAA)

    Farhad Ghaffari

  17. Navier-Stokes solutions about the F/A-18 forebody-LEX configuration

    Article • January 1989, American Institute of Aeronautics and Astronautics (AIAA)

    Farhad Ghaffari

  18. An analytical method for the ditching analysis of an airborne vehicle

    Article • June 1988, American Institute of Aeronautics and Astronautics (AIAA)

    Farhad Ghaffari