Early flights indicated tendency for airplane to "Dutch Roll" at lower indicated air speeds; elimination of this condition accomplished by use of servomechanism termed "yaw damper"; method of analysis based upon airplane inverse frequency response characteristics has been used, from which airplane stability has been obtained.


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    Title :

    Investigation of lateral dynamic stability in XB-47 airplane


    Additional title:

    J Aeronautical Sciences


    Contributors:
    White, R.J. (author)


    Publication date :

    1950


    Size :

    16 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :