Spray rig developed by Canadian National Research Council for in-flight study of phenomenon and testing of protective systems; ice accretion on main rotor blades; primary effect is increase in drag, resulting in drop in rotor rpm; secondary effects include vibration, damage due to flying ice, and throttle limitation; icing on other components; means of protection suggested.


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    Title :

    Some aspects of helicopter icing


    Additional title:

    Can Aeronautical J


    Contributors:

    Published in:

    Publication date :

    1957


    Size :

    11 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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