Measurements in wind tunnel yield data for validation of computations. Report describes experimental investigation of three-dimensional interaction of helicopter rotor blade with vortex like that generated by preceeding rotor blade. Provides theoretical aerodynamicists with data for validation of computer simulations of aerodynamic flow.


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    Titel :

    Interaction Of A Helicopter Blade With A Vortex


    Beteiligte:
    Dunagan, Stephen (Autor:in) / Norman, Thomas (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.09.1989



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


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