Experimental cruise flight data files from a wind tunnel test on a 1/4.622 Froude scale hingeless rotor, tilt rotor model are reported. Diverse data are presented; variables include parametric force, moment and blade fatigue loads, cruising flight speed, aircraft attitude, rotor control input, wing flap deflection, thrust load, and rotor RPM.


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    Title :

    Wind Tunnel Test on a 1/4.622 Froude Scale, Hingeless Rotor, Tilt Rotor Model, Volume 4


    Contributors:
    J. P. Magee (author)

    Publication date :

    1976


    Size :

    568 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English