Investigation of rotor contribution to stability derivatives of aircraft at high rotor inflow ratio conditions made; analytical expressions for evaluating rotor stability derivatives developed for hovering, transitional, and high speed flight regimes; error in estimating rotor derivatives by application of small angle assumption is determined.


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    Title :

    Rotor stability derivatives at high inflow ratio conditions for tilt rotor VTOL aircraft


    Additional title:

    Am Helicopter Soc -- J


    Contributors:
    Liu, D.T. (author)


    Publication date :

    1962


    Size :

    12 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :