To determine the aerodynamic loads on the structural elements of the mobile-deployable landing platform, numerical modeling of the turbulent flow of a viscous compressible gas induced by the rotation of the helicopter rotor is carried out. The flowfield around the helicopter is determined on the basis of numerical calculations, and the pressure distribution on the structural elements of the landing platform is discussed.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Simulation of Aerodynamic Loads on Structural Elements of Landing Platform whilst Helicopter Takeoff and Landing


    Weitere Titelangaben:

    Russ. Aeronaut.


    Beteiligte:

    Erschienen in:

    Russian Aeronautics ; 65 , 2 ; 297-305


    Erscheinungsdatum :

    2022-04-01


    Format / Umfang :

    9 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Vehicle-mounted folding helicopter takeoff and landing platform

    ZHU HAIQING / LI WANG / MEI ZHIYONG et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Optimization of helicopter takeoff and landing

    CERBE, T. / REICHERT, G. | AIAA | 1989




    TAKEOFF AND LANDING PLATFORM, METHOD FOR USING TAKEOFF AND LANDING PLATFORM, AND PROGRAM

    KOMINAMI ATSUSHI / ARAKI SOUJI | Europäisches Patentamt | 2021

    Freier Zugriff