Evaluation for small single rotor helicopter with various types of control feedback; effects of fuselage pitching moment characteristics on stability also evaluated; problem of maintaining stability with respect to velocity at high forward speeds.


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    Title :

    Helicopter longitudinal stability in forward flight with control feedback and fuselage aerodynamics


    Additional title:

    Am Helicopter Soc -- J


    Contributors:


    Publication date :

    1957


    Size :

    9 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :