Aircraft for sustained supersonic flight usually feature low aspect ratio wings with varying (reducing) leading edge sweep over the outer portion to achieve an adequate low-speed performance. A high-speed 'cruise' wing then becomes subject to mixed flows at low-speeds including strong Vortical flows.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Vortex Flow Dilemmas and Control on Wing Planforms on High Speed


    Contributors:
    R. K. Nangia (author) / A. Miller (author)

    Publication date :

    2003


    Size :

    15 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Wing planforms for high-speed flight

    Jones, R. T. | NTRS | 1976


    Vortex-lift prediction for complex wing planforms.

    BRADLEY, R. G. / SMITH, C. W. / BHATELEY, I. C. | AIAA | 1973


    Vortex Interactions above Multi-Swept Wing Planforms at Transonic Speeds

    Werner, Michael / Henne, Ulrich / Rein, Martin et al. | AIAA | 2024


    Flow Control over Trapezoidal-Wing Planforms with Sharp Edges

    Rullan, Jose / Vlachos, Pavlos / Telionis, Demetri | AIAA | 2006


    VTOL aircraft having multiple wing planforms

    KNOLL JONATHAN ANDREW / THOMPSON GEORGE MATTHEW / LOUIS MATTHEW EDWARD | European Patent Office | 2022

    Free access