All Stories

  1. Boundary-layer instability measurements on a cone at freestream Mach 3.5

    Article • Physics of Fluids, October 2021, American Institute of Physics

    Dr Rudolph A King

  2. Transition Induced by an Egg-Crate Roughness on a Flat Plate in Supersonic Flow

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

    Dr Rudolph A King

  3. 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

  4. LaRC Aerothermodynamic Ground Tests in Support of BOLT Flight Experiment

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

    Dr Rudolph A King, Dr. Beth Rieken

  5. Freestream Disturbance Effects on Boundary Layer Instability and Transition on the AFOSR BOLT Geometry

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

    Dr Rudolph A King

  6. Influence of a Backward-Facing Step on Swept-Wing Boundary-Layer Transition

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

    Dr. Meelan Choudhari, Dr Rudolph A King

  7. Interaction of a Backward-Facing Step and Crossflow Instabilities in Boundary-Layer Transition

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

    Dr Rudolph A King, Dr. Meelan Choudhari

  8. 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

  9. 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

  10. 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

  11. The Effect of Acoustic Forcing on Instabilities and Breakdown in Swept-Wing Flow Over a Backward-Facing Step

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

    Dr. Meelan Choudhari, Dr Rudolph A King

  12. Computations of Disturbance Amplification Behind Isolated Roughness Elements and Comparison with Measurements

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

    Dr. Meelan Choudhari, Dr Rudolph A King

  13. The Effect of Backward-facing Step Height on Instability Growth and Breakdown in Swept-Wing Boundary-Layer Transition

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

    Dr. Meelan Choudhari, Dr Rudolph A King

  14. The Interaction of a Backward-Facing Step and Crossflow Instabilities in Boundary-Layer Transition

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

    Dr. Meelan Choudhari, Dr Rudolph A King

  15. An Experimental Study of Roughness-Induced Instabilities in a Supersonic Boundary Layer

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

    Dr. Meelan Choudhari, Dr Rudolph A King

  16. Effects of Forward and Backward Facing Steps on the Crossflow Receptivity and Stability in Supersonic Boundary Layers

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

    Dr Rudolph A King