Study, carried out by Lockheed Aircraft Corp, and comparison made between teetering, offset hinge, and rigid rotor, led to helicopter concept incorporating rigid rotor for control power and simplicity in combination with control gyroscope to provide stability; details of full-scale vehicle and flight-test data; stress and vibration data; future programs. (See also Flight v 81 n 2764 Mar 1 1962 p 323-5)


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    Titel :

    Concept and development of simple, stable, and economical VTOL vehicle


    Weitere Titelangaben:

    Aerospace Eng


    Beteiligte:
    Hibbard, H.L. (Autor:in) / Heppe, R.R. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1962


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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