Explains the origins of rotor aerodynamic limits for helicopters including retreating and advancing blade limits. Examines the compounding of a helicopter for higher forward speed and reports the conclusions of a student project to design a rotorcraft capable of 300 knots and carrying a payload of 30 passengers.


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    Titel :

    The compound helicopter configuration and the helicopter speed trap


    Beteiligte:
    Newman, Simon (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.10.1997


    Format / Umfang :

    7 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





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