Perforation is proposed as an approach aiming to increase stability of subsonic flight vehicles under massive flow separation on a lateral surface and in a wake. Both experimental as well as numerical tests carried out at this early stage were aimed to estimate influence of perforation on flow structures as well as aerodynamic characteristics of the subsonic flight vehicles equipped with stabilizing disks, flares and flaps and, thus, operating under massive flow instability.


    Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Experimental and Numerical Modeling of Flow around Perforated Stabilizing Devices


    Contributors:


    Publication date :

    2013


    Size :

    8 Seiten





    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Numerical modeling of flow mixing and cooling processes in a perforated exhaust duct

    Kozlova, A. V. / Modorskii, V. Ya. / Sokolkin, Yu. V. et al. | Online Contents | 2014


    Numerical modeling of flow mixing and cooling processes in a perforated exhaust duct

    Kozlova, A. V. / Modorskii, V. Ya. / Sokolkin, Yu. V. et al. | Springer Verlag | 2014


    Experimental and Numerical Analyses of Perforated Corrugated Steel Shear Walls

    Nouri, Gholamreza / Rayegani, Arash / Nemati, Fariba et al. | Springer Verlag | 2023


    Stabilizing effects of a perforated splitter plate on a backwards-facing step

    Ormonde, Pedro C. / Cavalieri, André V. / Annes da Silva, Roberto G. et al. | AIAA | 2017


    Numerical and Experimental Study of Acoustic Damping Generated by Perforated Screens.

    Valter Bellucci / Peter Flohr / Christian Paschereit | AIAA | 2004