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


    Access

    Download


    Export, share and cite



    Title :

    Numerical optimization of helicopter rotor blade design for active twist control


    Contributors:


    Publication date :

    2007




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    Unknown




    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