From theoretical study it has been found that rates of roll within certain limits may cause instability if directional and longitudinal stabilities are different; if stabilities in both planes are equal, instability due to rolling will not occur; if rolling frequency is sufficiently high, rolling aircraft may be stable even if non-rolling aircraft is unstable in one plane.


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    Title :

    Effect of steady rolling on longitudinal and directional stability


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1948


    Size :

    36 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :