Rotor configuration; hovering problems; range; limitations to maximum flying speed; appendix considers optimum fuel weight ratio for horizontal flight of 100 mi. Before Inst Aeronautical Sciences, Toronto.


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    Title :

    Some aerodynamic problems in helicopter design


    Additional title:

    Aircraft Eng


    Contributors:

    Published in:

    Publication date :

    1952


    Size :

    5 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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