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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    Titel :

    Some aspects of helicopter icing


    Weitere Titelangaben:

    Can Aeronautical J


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    1957


    Format / Umfang :

    11 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Helicopter icing

    Saeed, B | Online Contents | 2010


    Helicopter Flight in Icing Conditions - Operational Aspects

    Lande, K. | British Library Conference Proceedings | 1996


    Helicopter Flight in Icing Conditions - Operational Aspects

    Lande, K. / American Helicopter Society / SAE | British Library Conference Proceedings | 1995


    Helicopter Icing Review

    A. A. Peterson / L. U. Dadone | NTIS | 1980


    Helicopter icing research

    Adams, R. I. | NTRS | 1978