All Stories

  1. Computational Study of Combustor Dilution Flow Interaction with Turbine Vanes

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

    Dr. Stephen P Lynch

  2. Three-Dimensional Boundary Layer in a Turbine Blade Passage

    Article • Journal of Propulsion and Power, July 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Stephen P Lynch

  3. Experimental Measurements of Turbulent Junction Flow Using High Speed Stereo PIV and IR Thermography

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

    Dr. Stephen P Lynch

  4. Combustor Dilution Hole Placement and Its Effect on the Turbine Inlet Flowfield

    Article • Journal of Propulsion and Power, May 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Stephen P Lynch, Michael Leonetti

  5. Experimental comparison of a traditionally built versus additively manufactured aircraft heat exchanger

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

    Dr. Stephen P Lynch

  6. A Computational Study of Combustor Dilution Flow Interaction with Turbine Vanes

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

    Dr. Stephen P Lynch

  7. Measurements and Predictions of the Three-Dimensional Boundary Layer in a Turbine Blade Passage

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

    Dr. Stephen P Lynch

  8. Time Resolved Stereo-PIV Measurements of the Horseshoe Vortex System in a Low Aspect Ratio Pin-Fin Array

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

    Dr. Stephen P Lynch