Report describes calculations of transonic airflows about wing in wind tunnel. Basic equations of flow used in study are Reynolds-averaged Navier-Stokes equations in strong conservation-law form. Equations of flow incorporated into finite-difference computer code called TNS (Transonic Navier-Stokes). Computational grid generated by solution of partial differential equations yielding smooth meshes conforming to surfaces of wing and wind tunnel.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Calculations Of Transonic Flow About A Wing


    Contributors:

    Published in:

    Publication date :

    1988-04-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :





    Improved Transonic Wing Flow Calculations Using Transition Correlations

    Gürdamar, Emre / Çete, Ruhsen / Aksel, Haluk et al. | AIAA | 2006


    Improved Transonic Wing Flow Calculations Using Transition Correlations

    Gurdamar, E. / Cete, R. / Aksel, H. et al. | British Library Conference Proceedings | 2006