From the time that wind tunnel wall interference was recognized to be significant, researchers have been developing methods to alleviate or account for it. Despite the best effort so far, it appears that no method is available which completely eliminates the effects due to the wind tunnel walls. This report discusses procedures developed for slotted wall and adaptive wall test sections of the Langley 0.3-m Transonic Cryogenic Tunnel (TCT) to assess and correct for the residual interference by methods consistent with the transonic nature of the tests.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Nonlinear Transonic Wall-Interference Assessment/Correction (WIAC) Procedures and Application to CAST-10 Airfoil Results from the NASA 0.3-M TCT 8- by 24-Inch Slotted Wall Test Section (SWTS)


    Contributors:
    C. R. Gumbert (author) / L. L. Green (author) / P. A. Newman (author)

    Publication date :

    1989


    Size :

    27 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English