Development of 33-ft diam, three-blade stowed rotor system which was employed for flight tests on modified Lockheed XH-51A compound helicopter, designated as CL 870; aeroelastic wind tunnel tests demonstrated feasibility of stowed-rotor concept relative to in-flight transition from compound helicopter mode to fixed-wind mode; evaluation of aeroelastic phenomena; applicability of methods of analysis are substantiated by correlations with specific results obtained in experiments; good agreement between calculated and measured results was established.


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    Titel :

    Analysis of stowed rotor aeroelastic characteristics


    Weitere Titelangaben:

    Am Helicopter Soc -- J


    Beteiligte:
    Donham, R.E. (Autor:in) / Harvick, W.P. (Autor:in)


    Erscheinungsdatum :

    1967


    Format / Umfang :

    24 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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