All Stories

  1. Experiments on Discrete Roughness Element Technology for Swept-Wing Laminar Flow Control

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

    Matthew W Tufts

  2. Crossflow Transition Acceleration with Plasma Actuators in Hypersonic Quiet Flow

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

    Matthew W Tufts

  3. Computational Investigation of Effective Trip Heights in Hypersonic Flows

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

    Matthew W Tufts

  4. Parabolized Stability Equation Analysis of Crossflow Instability on HIFiRE-5b Flight Test

    Article • Journal of Spacecraft and Rockets, November 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Matthew W Tufts

  5. Collaboration Between Flight Test, Ground Test, and Computation on HIFiRE-5

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

    Matthew W Tufts

  6. Computational Investigation of Step Excrescence Sensitivity in a Swept-Wing Boundary Layer

    Article • Journal of Aircraft, August 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Matthew W Tufts

  7. Computational Investigation of Step Excrescence Sensitivity in a Swept-Wing Boundary Layer

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

    Matthew W Tufts

  8. Flight Test Experiments on Discrete Roughness Element Technology for Laminar Flow Control

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

    Matthew W Tufts

  9. Effects of Step-Excrescence Location on Swept-Wing Transition

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

    Matthew W Tufts

  10. Design of an Infinite-Swept-Wing Glove for In-Flight Discrete-Roughness-Element Experiment

    Article • Journal of Aircraft, September 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Matthew W Tufts

  11. Effects of Step Excrescences on a Swept Wing in a Low-Disturbance Wind Tunnel

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

    Matthew W Tufts