This report presents the results of a propeller vibratory stress survey on the Fairey Gannet aircraft aimed at giving an assessment of the difference in vibratory response between single and counter-rotating propeller operation in angular inflow. The survey showed that counter-rotating operation of the propeller had the effect of increasing the IP response of the rear propeller by approximately 25 percent over comparable single-rotation operation while counter-rotating operation did not significantly influence the IP response of the front propeller.


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    Titel :

    Effect of Angular Inflow on the Vibratory Response of a Counter-Rotating Propeller


    Beteiligte:
    J. E. Turnberg (Autor:in) / P. C. Brown (Autor:in)

    Erscheinungsdatum :

    1985


    Format / Umfang :

    75 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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