The vibration of a helicopter has several different sources, such as the rotor, engine and transmission system. This creates a number of problems with performance, for example poor manoeuvrability, discomfort of the pilot, low fatigue life of the structural components, and, consequently, high operating costs. First published online: 14 Oct 2010


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Numerical optimization of helicopter rotor blade design for active twist control


    Beteiligte:
    Andrejs Kovalovs (Autor:in) / Evgeny Barkanov (Autor:in) / Sergejs Gluhihs (Autor:in)


    Erscheinungsdatum :

    2007




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Unbekannt




    Twist Optimization of a Helicopter Rotor Blade Using Support Vector Regression

    Ozyilmaz, Emin B. / Kaya, Mustafa / Elfarra, Munir A. | TIBKAT | 2023


    Twist Optimization of a Helicopter Rotor Blade Using Support Vector Regression

    Ozyilmaz, Emin B. / Kaya, Mustafa / Elfarra, Munir A. | AIAA | 2023




    Active Twist Control of Smart Helicopter Rotor -- A Survey

    Thakkar, Dipali | Online Contents | 2005