A multi-zonal, unified, space/time marching method has been used to solve the Euler and Reynolds-averaged Navier-Stokes equations for supersonic flow past an Advanced Short Take-Off and Vertical Landing (ASTOVL) aircraft configuration. Lift, drag and pitching moment values obtained from the computations compare well with wind-tunnel measurements. The calculations demonstrate the capability of the method used to accurately predict design parameters such as lift, drag and pitching moment for very complex aircraft configurations.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Supersonic flow computations for an ASTOVL aircraft configuration


    Beteiligte:

    Kongress:

    AIAA Applied Aerodynamics Conference ; 1990 ; Portland, OR, United States


    Erscheinungsdatum :

    01.01.1990


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :




    ASTOVL aircraft concept

    Online Contents | 1996


    The Direct Lift ASTOVL Aircraft

    Brower, D. / American Helicopter Society | British Library Conference Proceedings


    Internal reversing flow in a tailpipe offtake configuration for ASTOVL aircraft

    McArdle, Jack G. / Esker, Barbara S. / Rhodes, James A. | AIAA | 1994