Several important configuration features are discussed relative to adaptation of Lockheed XH-51A rigid rotor to compound research flight vehicle; testing undertaken to support XH-51A compound program included flight test of both three and four-bladed rotor helicopter; flight tests of compound research vehicle through Phase I and Phase II and results in terms of measured data and handling characteristics are presented; flight tests peculiar to compound aircraft are discussed along with pilot qualitative comments.


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    Titel :

    XH-51a compound research flight test program


    Weitere Titelangaben:

    Can Aeronatuics Space J


    Beteiligte:
    Segner, D.R. (Autor:in)


    Erscheinungsdatum :

    1967


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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