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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    Titel :

    Effect of steady rolling on longitudinal and directional stability


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Phillips, W.H. (Autor:in)


    Erscheinungsdatum :

    1948


    Format / Umfang :

    36 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :