All Stories

  1. Input/output analysis of a Mach-6 cooled-wall hypersonic boundary layer using the One-Way Navier-Stokes (OWNS) Equations

    Article • June 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Matthew Lakebrink

  2. Hypersonic Tripped Boundary Layer Measurements using FLEET Velocimetry

    Article • June 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Richard B Miles, Matthew Lakebrink, Boris Leonov

  3. Benchmark Characterization of Separated Flow Over Smooth Gaussian Bump

    Article • June 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Patrick Gray, Professor Thomas C. Corke, Matthew Lakebrink

  4. Experimental and Numerical Investigation of Active Flow Control of a Serpentine Diffuser

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

    George Woo, Matthew Lakebrink, Mori Mani

  5. Controlled Flow Dynamics in a Serpentine Diffuser with a Cowl Inlet

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

    George Woo, Matthew Lakebrink, Mori Mani

  6. Toward Improved Turbulence-Modeling Techniques for Internal-Flow Applications

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

    Matthew Lakebrink, Mori Mani

  7. Numerical Investigation of Dynamic Distortion and Flow Control in a Serpentine Diffuser

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

    Matthew Lakebrink

  8. Optimization of a Mach-6 Quiet Wind-Tunnel Nozzle

    Article • Journal of Spacecraft and Rockets, September 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Kevin G Bowcutt, Matthew Lakebrink

  9. Numerical Investigation of Fluidic Oscillator Flow Control in an S-Duct Diffuser

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

    Mori Mani, Matthew Lakebrink

  10. Experimental and Numerical Investigation of Controlled Flow Distortion in a Subsonic Offset Diffuser by Trapped Vorticity

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

    Mori Mani, Matthew Lakebrink, George Woo

  11. Traveling Crossflow Wave Predictions on the HIFiRE-5 at Mach 6: Stability Analysis vs. Quiet Tunnel Data

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

    Matthew Lakebrink