The leading-edge-suction analogy of Polhamus, which has been successful in the prediction of vortex lift characteristics on wings with pointed tips at subsonic and supersonic speeds, has recently been extended to account for the vortex flow characteristics for wings with side edges. Comparisons of experimental data and other currently used methods with the extended method are made for wings having side edges at subsonic and supersonic speeds. Recent data obtained for a low-aspect-ratio cropped-delta wing with various amounts of asymmetrical tip rake, simulating a roll control device, are also presented.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Prediction of vortex flow characteristics of wings at subsonic and supersonic speeds


    Contributors:

    Conference:

    American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting ; 1975 ; Pasadena, CA


    Publication date :

    1975-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English


    Keywords :




    Vortex Interaction Characteristics of Multiswept Wings at Subsonic Speeds

    Ghoreyshi, Mehdi / Fagley, Casey / Seidel, Jürgen | AIAA | 2023


    Canard-wing vortex interactions at subsonic through supersonic speeds

    Erickson, Gary E. / Schreiner, John A. / Rogers, Lawrence W. | NTRS | 1990


    Computational Study of Vortex Interaction Characteristics of Multi-Swept Wings at Subsonic Speeds

    Ghoreyshi, Mehdi / Herman, Carter c. / Smiley, Trevor D. et al. | AIAA | 2022