Wing tunnel test data on a 1/4.622 Froude scale, hingeless rotor, tilt rotor mode are reported for all potential flight conditions through hover and a wide envelope of transitions. A mathematical model was used to describe the rotor system in real time simulation by means of regression analyses. Details of the model, test program and data system are provided together with four data files for hover and transition. Diverse data are presented; variables include parametric force, moment and blade fatigue loads, flight range, airspeed, aircraft attitude, rotor control inputs, wing flap deflection, thrust loads and rotor RPM.


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    Titel :

    Wind Tunnel Test on a 1/4.622 Froude Scale, Hingeless Rotor, Tilt Rotor Model, Volume 1


    Beteiligte:
    J. P. Magee (Autor:in) / H. R. Alexander (Autor:in)

    Erscheinungsdatum :

    1976


    Format / Umfang :

    779 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch