All Stories

  1. Direct Numerical Simulation of Nozzle-Wall Pressure Fluctuations in a Mach 8 Wind Tunnel

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

    Lian Duan, Gary Nicholson, Junji Huang

  2. Stabilization of a Swept-Wing Boundary Layer by Discrete Roughness Elements at High Reynolds Numbers

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

    Lian Duan, Gary Nicholson

  3. Direct Numerical Simulation of Receptivity to Roughness in a Swept-Wing Boundary Layer at High Reynolds Numbers

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

    Gary Nicholson