All Stories

  1. Reynolds Number Effects on the Surface Pressures on a 5.2%-Scale High Lift Common Research Model

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

    Melissa Rivers Rivers

  2. 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

  3. National Transonic Facility Public Geometry Release and Summary

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

    Melissa Rivers Rivers

  4. Test Summary of the NASA High-Lift Common Research Model Half-Span at QinetiQ 5-Metre Pressurized Low-Speed Wind Tunnel

    Article • June 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Melissa Rivers Rivers, Ashley Evans

  5. NASA Common Research Model: A History and Future Plans

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

    Melissa Rivers Rivers

  6. Evaluation of Cryogenic Force Balance Calibration Methodologies Relative to Wind Tunnel Results

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

    Devin Burns, Melissa Rivers Rivers

  7. Preliminary Results from an Experimental Assessment of a Natural Laminar Flow Design Method

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

    Melissa Rivers Rivers

  8. Experimental Investigation of the NASA Common Research Model with a Natural Laminar Flow Wing in the NASA Langley National Transonic Facility

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

    Melissa Rivers Rivers

  9. NASA Common Research Model: A History and Future Plans

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

    Melissa Rivers Rivers

  10. Retrospective on the Common Research Model for Computational Fluid Dynamics Validation Studies

    Article • Journal of Aircraft, July 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Melissa Rivers Rivers, Dr Richard A Wahls

  11. Computational Fluid Dynamics Analyses for the High-Lift Common Research Model Using the USM3D and FUN3D Flow Solvers

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

    Melissa Rivers Rivers

  12. Comparison of the NASA Common Research Model European Transonic Wind Tunnel Test Data to NASA Test Data (Invited)

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

    Melissa Rivers Rivers

  13. Investigation of Aeroelastic Effects on the NASA Common Research Model

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

    Stefan Keye, Melissa Rivers Rivers

  14. NASA Common Research Model Test Envelope Extension with Active Sting Damping at NTF

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

    Dr sundareswara balakrishna, Melissa Rivers Rivers