Flight-test results which describe flying-quality factors related to the fan-in-fin yaw control concept as utilized on a pre-production version of a European helicopter are presented. Design compromises to be considered with this concept are also presented. The large, fixed vertical fin associated with the fan-in-fin system was helpful in maneuvering flight, but introduced several flying-quality problems when combined with the fan.


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    Titel :

    Flight investigation of effects of a fan-in-fin yaw control concept on helicopter flying-quality characteristics


    Beteiligte:
    Kelley, H. L. (Autor:in) / West, T. C. (Autor:in)

    Erscheinungsdatum :

    1974-04-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :




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