This paper will demonstrate how to adapt fixed wing lift/drag equations to analyze rotary wings as airfoils. This Airfoil method is validated by analysis of eight radio controlled helicopters and quad-copters, which are flown at a hover for a known time duration.


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    Titel :

    Airfoil Method for Rotary Wing Analysis Using Modified Lift and Drag Equations


    Beteiligte:
    T. Kraeutner (Autor:in)

    Erscheinungsdatum :

    2021


    Format / Umfang :

    89 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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