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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    Title :

    The compound helicopter configuration and the helicopter speed trap


    Contributors:

    Published in:

    Publication date :

    1997-10-01


    Size :

    7 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English





    The compound helicopter configuration and the helicopter speed trap

    Newman, S. | British Library Online Contents | 1997


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