The rotorcraft dynamics analysis was used to predict the aeroelastic responses of a representative X-wing model with a 10 ft diameter rotor. The aeroelastic methodology used and the tests and assumptions involved are reviewed. Results are reported on the findings concerning control power and higher harmonic control in hover, transition flight, vibratory loads at forward speed, and responses in conversion. It is concluded that the analysis can give satisfactory predictions of X-wing behavior.


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    Titel :

    Prediction of Aeroelastic Response of a Model X-Wing Rotor


    Beteiligte:
    R. Dopher (Autor:in) / J. E. Duh (Autor:in)

    Erscheinungsdatum :

    1987


    Format / Umfang :

    16 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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