All Stories

  1. Comparison of OVERFLOW Computational and Experimental Results of the CobraMRV Mars Entry Vehicle Concept During Supersonic Retropropulsion

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

    Thomas Pulliam

  2. Comparison of OVERFLOW Computational and Experimental Results for a Blunt Mars Entry Vehicle Concept During Supersonic Retropropulsion

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

    Thomas Pulliam

  3. CFD Comparisons with Updated NASA Juncture Flow Data

    Article • January 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Thomas Pulliam

  4. Improvements to the Quadratic Constitutive Relation Based on NASA Juncture Flow Data

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

    Thomas Pulliam

  5. High-Lift Simulations of the Japan Aerospace Exploration Agency Standard Model

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

    Thomas Pulliam

  6. Overflow Juncture Flow Computations Compared with Experimental Data

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

    Thomas Pulliam

  7. Contributions to the Sixth Drag Prediction Workshop Using Structured, Overset Grid Methods

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

    Thomas Pulliam

  8. Time-Spectral Method for Overlapping Meshes

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

    Thomas Pulliam, Joshua Leffell

  9. CFD Analysis in Advance of the NASA Juncture Flow Experiment

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

    Thomas Pulliam

  10. Boundary Condition Study for the Juncture Flow Experiment in the NASA Langley 14x22-Foot Subsonic Wind Tunnel

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

    Thomas Pulliam

  11. Contributions to the 6th AIAA CFD Drag Prediction Workshop Using Structured Grid Methods

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

    Thomas Pulliam

  12. Computations of Torque-Balanced Coaxial Rotor Flows

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

    Thomas Pulliam

  13. Stability Analysis of Dual-time Stepping

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

    Thomas Pulliam

  14. Near-Body Grid Adaption for Overset Grids

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

    Thomas Pulliam

  15. Computational Analysis of Multi-Rotor Flows

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

    Thomas Pulliam

  16. Comparison of Experimental Surface and Flow Field Measurements to Computational Results of the Juncture Flow Model (JFM)

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

    Thomas Pulliam

  17. Effect of Turbulence Modeling on Hovering Rotor Flows

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

    Thomas Pulliam

  18. Drag Prediction for the Common Research Model Using CFL3D and OVERFLOW

    Article • Journal of Aircraft, July 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Thomas Pulliam

  19. High Lift OVERFLOW Analysis of the DLR F11 Wind Tunnel Model

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

    Thomas Pulliam

  20. Time-Spectral Rotorcraft Simulations on Overset Grids

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

    Thomas Pulliam, Joshua Leffell

  21. Fundamental Algorithms in Computational Fluid Dynamics

    Article • January 2014, Springer Science + Business Media

    Thomas Pulliam

  22. Fundamentals of Computational Fluid Dynamics

    Article • January 2001, Springer Science + Business Media

    Thomas Pulliam

  23. Recent enhancements to OVERFLOW

    Article • January 1997, American Institute of Aeronautics and Astronautics (AIAA)

    Thomas Pulliam

  24. A computational challenge - Euler solution for ellipses

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

    Thomas Pulliam

  25. Artificial dissipation models for the Euler equations

    Article • AIAA Journal, December 1986, American Institute of Aeronautics and Astronautics (AIAA)

    Thomas Pulliam

  26. Implicit solution methods in computational fluid dynamics

    Article • Applied Numerical Mathematics, December 1986, Elsevier

    Thomas Pulliam