New method of boundary control considers flexible aerodynamic surface as possible means of delaying transition and reducing skin-friction drag; results of analytical study on boundary-layer instability and transition in incompressible Blasius-flow over flexible surface are presented; simple flexible skin model consisting of taut membrane and elastic base is considered, and steps of computation procedure are given; potential fields of application of flexible skins would be in sailplanes, helicopters, small and medium subsonic airplanes, hydrofoils, torpedoes, speed boats, and miniature submarines.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Possibilities of drag reduction by use of flexible skin


    Weitere Titelangaben:

    J Aircraft


    Beteiligte:

    Erschienen in:

    Journal of Aircraft ; 4 , n 3 ; p 186-192


    Erscheinungsdatum :

    1967


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




    Self-adaptive bionic piezoelectric scale rigid-flexible integrated drag reduction skin

    ZHANG LU / ZHAO XIAOXUE / LYU MENGFEI et al. | Europäisches Patentamt | 2024

    Freier Zugriff


    Microstructured Hydrophobic Skin for Hydrodynamic Drag Reduction

    Ashwin Balasubramanian / Adam Miller / Othon Rediniotis | AIAA | 2004