All Stories

  1. Upstream Influence in Shock Wave/Transitional Boundary Layer Interactions at Mach 1.8

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

    E. Lara Lash

  2. Exploration of Upstream Influence and the Role of Shock Generator Geometry in Shock Wave/Transitional Boundary Layer Interactions at Mach 1.8 Edge Conditions

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

    E. Lara Lash

  3. Preliminary Unsteady Characterization of Shock Wave/Boundary Layer Interactions on a 4% Scale SLS Model using uPSP and Shadowgraph

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

    E. Lara Lash

  4. Shockwave/Boundary-Layer Interaction Studies Performed in the NASA Langley 20-Inch Mach 6 Air Tunnel

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

    E. Lara Lash

  5. Shockwave/Boundary-Layer Interaction Studies Performed in the NASA Langley 20-Inch Mach 6 Air Tunnel

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

    E. Lara Lash

  6. Investigating Unsteady Dynamics of Cylinder-Induced Shock-Wave/Transitional Boundary-Layer Interactions

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

    E. Lara Lash

  7. Image-Based Analysis of Shock-Wave/Boundary-Layer Interaction Unsteadiness

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

    E. Lara Lash

  8. Study of the Dynamics of Transitional Shock Wave-Boundary Layer Interactions using Optical Diagnostics

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

    Dr. Christopher S Combs, E. Lara Lash

  9. Experimental Investigation of a Cylinder-Induced Transitional Shock Wave-Boundary Layer Interaction

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

    Dr. Christopher S Combs, E. Lara Lash

  10. Investigation of a Cylinder-Induced Transitional Shock Wave-Boundary Layer Interaction using Laser Diagnostics

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

    Dr. Christopher S Combs, E. Lara Lash

  11. Developing an Image-Based Analysis of the Dynamics of Transitional Shock Wave-Boundary Layer Interactions

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

    Dr. Christopher S Combs, E. Lara Lash

  12. Assessment of Aerospike Nozzle for Single-Stage to Orbit Flight

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

    Dr. Trevor M. Moeller, E. Lara Lash