Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Computational Investigation of the Effect of Sweep on a Pitching Finite-Aspect-Ratio Wing (AIAA 2018-0357)


    Contributors:

    Conference:

    Aerospace sciences meeting ; 2018 ; Kissimmee, FL



    Publication date :

    2018-01-01


    Size :

    23 pages



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Experimental Investigation of the Effect of Sweep on a Pitching Finite-Aspect-Ratio Wing

    Ullah, Al Habib / Fabijanic, Charles / Refling, William et al. | AIAA | 2021


    Effect of Sweep on Dynamic Stall of a Pitching Finite-Aspect-Ratio Wing

    Visbal, Miguel R. / Garmann, Daniel J. | AIAA | 2019


    Control of Dynamic Stall Over a Pitching Finite-Aspect-Ratio Wing (AIAA 2017-4118)

    Visbal, Miguel R. / Garmann, Daniel J. | British Library Conference Proceedings | 2017


    EXPERIMENTAL INVESTIGATION OF THE EFFECT OF SWEEP ON A PITCHING FINITEASPECT-RATIO WING

    Ullah, Al Habib / Fabijanic, Charles / Refling, William et al. | TIBKAT | 2021