A lifting surface theory has been developed for a helicopter rotor in forward flight for incompressible flow. The method utilized the concept of the linearized acceleration potential and make use of the vortex lattice procedures. Results in terms of lift coefficient slope for several forward flight conditions are given.


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    Titel :

    Lifting surface theory for a helicopter rotor in forward flight


    Beteiligte:
    Runyan, H. L. (Autor:in) / Tai, H. (Autor:in)

    Erscheinungsdatum :

    01.01.1983


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


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    Aerodynamic prediction of helicopter rotor in forward flight using blade element theory

    M.F. Yaakub / A.A. Wahab / A. Abdullah et al. | DOAJ | 2017

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