Time histories of rolling velocity and angle of sideslip are obtained by application of Fourier transform to solve lateral equations of motion; time histories, calculated by using constant values for stability derivatives, are presented for comparison; results show that frequency effects of latter can cause considerable changes in predicted airplane motions.


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    Title :

    Analysis of dynamic lateral stability of delta-wing airplane with frequency-dependent stability derivatives


    Additional title:

    NASA -- Tech Note


    Contributors:
    Brown, A.E. (author) / Schy, A.A. (author)


    Publication date :

    1959


    Size :

    44 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :