The report presents the results of a flight test program on the Piasecki Model 16H-1A shaft-driven compound helicopter. The main components of the Model 16H-1A aircraft included: an H-21 articulated rotor, a wing with controllable flaperons and a shrouded pusher propeller. The aircraft was powered by a single T58-8 turbine engine. Aircraft performance, flying qualities, vibration and lift distribution between main rotor and wing were investigated over a level flight speed range of 0 to 167 knots and dive speeds up to 195 knots. (Author)


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    Titel :

    16H-1A Flight Test Research Program


    Beteiligte:
    D. N. Meyers (Autor:in) / L. V. Tompkins (Autor:in) / J. H. Goldberg (Autor:in)

    Erscheinungsdatum :

    1968


    Format / Umfang :

    399 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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