Computer codes for the design and analysis of transonic airfoils are considered. The design code relies on the method of complex characteristics in the hodograph plane to construct shockless airfoil. The analysis code uses artificial viscosity to calculate flows with weak shock waves at off-design conditions. Comparisons with experiments show that an excellent simulation of two dimensional wind tunnel tests is obtained. The codes have been widely adopted by the aircraft industry as a tool for the development of supercritical wing technology.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Transonic airfoil codes


    Beteiligte:


    Erscheinungsdatum :

    01.01.1979


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Transonic Airfoil Analysis

    Holst, T. L. / Dougherty, F. C. / Gundy, K. L. et al. | NTRS | 1984



    Transonic airfoil design

    CAHN, M. S. / GARCIA, J. R. | AIAA | 1971


    Transonic Airfoil Development

    Whitcomb, R. T. | NTRS | 1983


    Transonic airfoil design code

    Bauer, F. / Garabedian, P. / Korn, D. | NTRS | 1980