A genetic algorithm coupled with a simplified acoustic analysis was used to generate low-noise rotor blade designs. The model includes thickness, steady loading and blade-vortex interaction noise estimates. The paper presents solutions for several variations in the fitness function, including thickness noise only, loading noise only, and combinations of the noise types. Preliminary results indicate that the analysis provides reasonable assessments of the noise produced, and that genetic algorithm successfully searches for 'good' designs. The result show that, for a given required thrust coefficient, proper blade design can noticeably reduce the noise produced at some expense to the power requirements.


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    Titel :

    Acoustic design of rotor blades using genetic algorithm


    Weitere Titelangaben:

    Die akustische Auslegung von Rotorblättern mittels eines genetischen Algorithmus


    Beteiligte:
    Wells, V.L. (Autor:in) / Han, A.Y. (Autor:in) / Crossley, W.A. (Autor:in)


    Erscheinungsdatum :

    1995


    Format / Umfang :

    10 Seiten, 7 Bilder, 5 Tabellen, 14 Quellen



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Acoustic Design of Rotor Blades Using A Genetic Algorithm

    V. L. Wells / A. Y. Han / W. A. Crossley | NTRS | 1995


    Acoustic Design of Rotor Blades Using a Genetic Algorithm

    Wells, V. L. / Han, A. Y. / Crossley, W. A. et al. | British Library Conference Proceedings | 1995




    AIAA-2001-1605 Using a Genetic Algorithm for Structural Topology Design of Helicopter Rotor Blades

    Fanjoy, D. / Crossley, W. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2001