The utility of the cryogenic high Reynolds number test facility as a production tunnel is evaluated. Aerodynamic performance evaluation, numerical wing design verification, and high Reynolds number theoretical extensions are considered. A priority ranking of NTF uses from an airframe development viewpoint is presented.


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    Title :

    Aircraft design using the National Transonic Facility


    Contributors:
    Bonner, E. (author)


    Publication date :

    1981-09-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English






    The National Transonic Facility

    Holmes, Harlan K. | IEEE | 1986



    The National Transonic Facility

    Holmes, H. K. | NTRS | 1986