All Stories

  1. Design of a Crossflow Attenuated Natural Laminar Flow Flight Test Article

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

    Lewis Owens

  2. Supersonic Crossflow Transition Control in Ground and Flight Tests

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

    Lewis Owens, Dr Rudolph A King

  3. Receptivity and Forced Response to Acoustic Disturbances in High-Speed Boundary Layers

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

    Dr Rudolph A King, Lewis Owens

  4. Comparison of Sweeping Jet Actuators with Different Flow-Control Techniques for Flow-Separation Control

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

    Lewis Owens

  5. Receptivity and Forced Response to Acoustic Disturbances in High-Speed Boundary Layers

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

    Dr Rudolph A King, Lewis Owens

  6. Measurements in a Transitioning Cone Boundary Layer at Freestream Mach 3.5

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

    Lewis Owens, Dr Rudolph A King

  7. Flow Separation Control Over a Ramp Using Sweeping Jet Actuators

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

    Lewis Owens

  8. Flow Disturbance and Surface Roughness Effects on Cross-Flow Boundary-Layer Transition in Supersonic Flows

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

    Lewis Owens

  9. Off-Body Boundary-Layer Measurement Techniques Development for Supersonic Low-Disturbance Flows

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

    Lewis Owens

  10. High-Speed Boundary-Layer Transition Induced by an Isolated Roughness Element

    Article • June 2010, American Institute of Aeronautics and Astronautics (AIAA)

    Lewis Owens

  11. Boundary-Layer-Ingesting Inlet Flow Control

    Article • Journal of Aircraft, July 2008, American Institute of Aeronautics and Astronautics (AIAA)

    Lewis Owens

  12. Reynolds Number Effects on Off-Design Stability and Control Characteristics of Supersonic Transports

    Article • Journal of Aircraft, January 2007, American Institute of Aeronautics and Astronautics (AIAA)

    Lewis Owens

  13. Boundary-Layer-Ingesting Inlet Flow Control

    Article • January 2006, American Institute of Aeronautics and Astronautics (AIAA)

    Lewis Owens

  14. Optimal Design of Passive Flow Control for a Boundary-Layer-Ingesting Offset Inlet Using Design-of-Experiments

    Article • January 2006, American Institute of Aeronautics and Astronautics (AIAA)

    Lewis Owens

  15. Numerical Modeling of Flow Control in a Boundary-Layer-Ingesting Offset Inlet Diffuser at Transonic Mach Numbers

    Article • January 2006, American Institute of Aeronautics and Astronautics (AIAA)

    Lewis Owens

  16. Off-Design Reynolds Number Effects for a Supersonic Transport

    Article • Journal of Aircraft, November 2005, American Institute of Aeronautics and Astronautics (AIAA)

    Lewis Owens

  17. Numerical Modeling of Active Flow Control in a Boundary Layer Ingesting Offset Inlet

    Article • June 2004, American Institute of Aeronautics and Astronautics (AIAA)

    Lewis Owens

  18. Active Flow Control on a Boundary-Layer-Ingesting Inlet

    Article • January 2004, American Institute of Aeronautics and Astronautics (AIAA)

    Lewis Owens

  19. Advancement of Semispan Testing at the National Transonic Facility

    Article • Journal of Aircraft, March 2002, American Institute of Aeronautics and Astronautics (AIAA)

    Lewis Owens

  20. Reynolds number effects on the stability and control characteristics of a supersonic transport

    Article • January 2002, American Institute of Aeronautics and Astronautics (AIAA)

    Lewis Owens

  21. Reynolds number effects on leading edge radius variations of a supersonic transport at transonic conditions

    Article • June 2001, American Institute of Aeronautics and Astronautics (AIAA)

    Lewis Owens

  22. Reynolds number effects on a supersonic transport at subsonic high-lift conditions

    Article • January 2001, American Institute of Aeronautics and Astronautics (AIAA)

    Lewis Owens

  23. Reynolds number effects on a supersonic transport at transonic conditions

    Article • January 2001, American Institute of Aeronautics and Astronautics (AIAA)

    Lewis Owens