An airfoil design procedure is described that was incorporated into an existing 2-D Navier-Stokes airfoil analysis method. The resulting design method, an iterative procedure based on a residual-correction algorithm, permits the automated design of airfoil sections with prescribed surface pressure distributions. The inverse design method and the technique used to specify target pressure distributions are described. It presents several example problems to demonstrate application of the design procedure. It shows that this inverse design method develops useful airfoil configurations with a reasonable expenditure of computer resources.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Airfoil design method using the Navier-Stokes equations


    Beteiligte:
    Malone, J. B. (Autor:in) / Narramore, J. C. (Autor:in) / Sankar, L. N. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1991-03-01



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Airfoil design using the Navier-Stokes equations

    EYI, S. / HAGER, J. / LEE, K. | AIAA | 1993


    Airfoil design method using the Navier-Stokes equations

    MALONE, J. B. / NARRAMORE, J. C. / SANKAR, L. N. | AIAA | 1991




    Efficient Airfoil Design Method Using the Navier-Stokes Equations

    J. B. Malone / J. C. Narramore / L. N. Sankar | NTIS | 1990