All Stories

  1. The Role of Boundary-Layer Thickness on Cylinder-Generated Shock-Wave/Turbulent Boundary-Layer Interactions, Part II: Experiments

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

    Dr. Christopher S Combs

  2. Simulation of Transitional Shockwave/Boundary-Layer Interaction Using Advanced RANS-based Modeling

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

    Dr. Christopher S Combs

  3. Investigation of the Effects of Ablation-Induced Roughness on Supersonic Flows

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

    Dr. Christopher S Combs

  4. Limiting Cases for Cylinder-Induced Shock Wave/Boundary Layer Interactions

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

    Dr. Christopher S Combs

  5. 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

  6. Heat-Shield Ablation Visualized Using Naphthalene Planar Laser-Induced Fluorescence

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

    Dr. Christopher S Combs, Dr Paul M Danehy

  7. 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

  8. Numerical Simulations of a Cylinder-Induced Shock Wave/Boundary Layer Interaction

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

    Dr. Christopher S Combs

  9. 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

  10. 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

  11. An Investigation of the Role of an Upstream Burst Diaphragm on Flow Quality within a Ludwieg Tube using RANS

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

    Dr. Christopher S Combs

  12. Scalar and velocity measurements in a Mach 5 boundary layer

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

    Dr. Christopher S Combs

  13. Measurements of Ablation-Products Transport in a Mach 5 Turbulent Boundary Layer using Naphthalene PLIF

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

    Dr. Christopher S Combs

  14. Development of Naphthalene PLIF for Visualizing Ablation Products from a Space Capsule Heat Shield

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

    Dr Paul M Danehy, Dr. Christopher S Combs