The objectives of this program were to document the reduction in height-velocity restrictions for autorotational landings, the increased transient performance and maneuver capability using modified flight techniques, and the handling qualities of a modified OH-58A helicopter with a High Energy Rotor System (HERS). The rotor incorporated increased chord blades and provision for three different tip weights resulting in Lock number variations of 2.61, 3.14, and 5.43.


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    Titel :

    Flight Test Evaluation of the High Inertia Rotor System


    Beteiligte:
    L. W. Dooley (Autor:in) / R. D. Yeary (Autor:in)

    Erscheinungsdatum :

    1979


    Format / Umfang :

    121 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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