All Stories

  1. NASA 5.2%-Scale Semispan High Lift Common Research Model (CRM-HL) High Reynolds Number Wind Tunnel Test in the National Transonic Facility (NTF)

    Article • July 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Courtney Winski, Melissa Rivers Rivers

  2. Development of NASA 2.7% Semispan and Full Span High Lift Common Research Models (CRM-HL)

    Article • July 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Courtney Winski

  3. Reynolds Number Effects on a 5.2%-Scale High Lift Common Research Model

    Article • January 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Courtney Winski

  4. NASA 5.2%-Scale Semispan High Lift Common Research Model Wind Tunnel Test at the 14- by 22-Foot Subsonic Tunnel

    Article • January 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Courtney Winski

  5. Development of NASA 5.2%-Scale Semispan High Lift Common Research Model

    Article • January 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Courtney Winski