Small-scalefixed-pitch propellers especially on multicopter configurations experience higher angles of attack than on usual aircraft configurations. In order to improve their aerodynamic efficiency, a better understanding of the occurringflow-fields under such non-axial inflow conditions is required. Therefore, an isolated small-scale propeller is operated at a range of inflow angles from zero to 180 degrees. Experimental data obtained by measurements of forces as well as a particle image velocimetry (PIV) are compared to numerical results generated by methods of different fidelity.


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    Titel :

    Systematic Investigation of a Fixed-Pitch Small-Scale Propeller under Non-Axial Inflow Conditions


    Beteiligte:
    Cerny, M. (Autor:in) / Herzog, N. (Autor:in) / Faust, J. (Autor:in) / Stuhlpfarrer, M. (Autor:in) / Breitsamter, C. (Autor:in)

    Erscheinungsdatum :

    2021


    Format / Umfang :

    10 pages



    Medientyp :

    Sonstige


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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