The results of a study of folding tilt rotor (stowed rotor) aircraft are presented. The effects of design cruise speed on the gross weight of a conceptual design stowed rotor aircraft are shown and a comparison is made with a conventional (non-folding) tilt rotor aircraft. A flight research stowed rotor design is presented. The program plans, including costs and schedules, are shown for the research aircraft development and a wind tunnel plan is presented for a full scale test of the aircraft. (Author)


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    Titel :

    V/STOL Tilt Rotor Aircraft Study. Volume 5: Definition of Stowed Rotor Research Aircraft


    Beteiligte:
    V. A. Soule (Autor:in)

    Erscheinungsdatum :

    1973


    Format / Umfang :

    134 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch