Aircraft constitutes next-generation rotary-wing research aircraft, aimed at providing technology base for rotary-wing aircraft having speed capabilities in 300 to 350 knot speed range; approach to program is to combine into one aircraft hover efficiency and downwash velocities of helicopter and high-speed efficiency of fixed-wing aircraft; to obtain desired speed, rotor drag in high-speed flight must be reduced or eliminated by altering mode of operation of rotor; possible solutions are considered.


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    Titel :

    Composite aircraft design


    Weitere Titelangaben:

    Am Helicopter Soc -- J


    Beteiligte:
    Ludi, L.H. (Autor:in)


    Erscheinungsdatum :

    1968


    Format / Umfang :

    10 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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