Optimization of L/D through minimizing induced drag through a detailed flow study together with force, pressure and vorticity measurements is considered. Flow visualization with neutral helium bubbles provides an excellent means of observing the effects of configuration changes.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Wing Tip Vortex Drag


    Contributors:


    Publication date :

    1975-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English


    Keywords :


    PASSIVE, ACTIVE AND ADAPTIVE SYSTEMS FOR WING VORTEX DRAG REDUCTION

    Ceron-Munoz, H.D. / Catalano, F.M. / Coimbra, R.F. et al. | British Library Conference Proceedings | 2008



    Wing Induced Drag

    Schmidt, Louis / Duren, R. | AIAA | 2002


    WING TIP STRUCTURE FOR SUPPRESSING LIFT LOSS DUE TO VORTEX DRAG GENERATED AT SIDE OF WING

    SHIBASAKI TAKENOBU | European Patent Office | 2017

    Free access

    Vortex Drag Revisited

    Butcher, Daniel / Le Good, Geoffrey / Howell, Jeff | SAE Technical Papers | 2023