All Stories

  1. Large Eddy Simulation of Rough Wall Hypersonic Turbulent Boundary Layers

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

    Doyle Knight

  2. Examination of Nonequilibirum Effects at High Mach Number and Stagnation Enthalpy for Double Cone Model

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

    Doyle Knight

  3. Large Eddy Simulation of Cold Wall Hypersonic Turbulent Boundary Layers

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

    Doyle Knight

  4. Flight Control of an Ogive Cylinder with Off-Axis Laser Discharge

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

    Doyle Knight

  5. Simulation of Turbulent Hypersonic Flow over a Cold Wall Flat Plate Using Large Eddy Simulation

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

    Doyle Knight, Nadia Kianvashrad

  6. Introduction to Special Issue on boundary layer transition

    Article • Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering, January 2020, SAGE Publications

    Doyle Knight

  7. Simulation of Hypersonic-Shock-Wave–Laminar-Boundary-Layer Interaction over Blunt Fin

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

    Doyle Knight

  8. Nonequilibrium Effects on Prediction of Aerothermodynamic Loading for a Double Cone

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

    Nadia Kianvashrad, Doyle Knight

  9. Flight Control Using Off-Axis Laser Discharge

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

    Nadia Kianvashrad, Dr Edward P DeMauro, Doyle Knight

  10. Shock-Shock Interaction over a Hemisphere in Hypersonic Flow

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

    Nadia Kianvashrad, Doyle Knight

  11. Simulation of Hypersonic Shock-Wave–Laminar-Boundary-Layer Interaction on Hollow Cylinder Flare

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

    Nadia Kianvashrad, Doyle Knight

  12. Simulation of Hypersonic Shock Wave Laminar Boundary Layer Interaction on Hollow Cylinder Flare

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

    Nadia Kianvashrad, Doyle Knight

  13. Assessment of CFD Capability for Hypersonic Shock Wave Boundary Layer Interactions, Part II

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

    Doyle Knight

  14. Shock Wave Boundary Layer Interaction in a Hypersonic Laminar Flow on a Hollow Cylinder Flare

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

    Doyle Knight

  15. Novel Technique to Determine SparkJet Efficiency

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

    Doyle Knight

  16. Assessment of CFD Capability for High Enthalpy Non-Equilibrium Flows with Strong Viscous-Inviscid Interaction

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

    Doyle Knight

  17. Numerical Prediction of Dynamics of Microwave Filament Interaction with Supersonic Combined Cylinder Bodies

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

    Doyle Knight

  18. Numerical Prediction of Dynamics of Interaction of Laser Discharge Plasma with a Hemisphere-Cylinder in a Supersonic Flow

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

    Doyle Knight

  19. Numerical Simulation of Energy Deposition in a Viscous Supersonic Flow Past a Hemisphere

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

    Doyle Knight

  20. Numerical Simulation of Energy Deposition in a Supersonic Flow Past a Hemisphere

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

    Doyle Knight

  21. Shock Wave Laminar Boundary Layer Interaction Over a Double Wedge in a High Mach Number Flow

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

    Doyle Knight