Investigation in connection with program to compute stability derivatives of certain specific aircraft and missiles; paper divided into three parts; curved flight path, zero rate of change of sideslip; straight flight path, rate of change of sideslip equals rate of yaw; rate of change of sideslip and yaw.


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    Title :

    Dynamic derivatives in yaw and sideslip of thin wings at supersonic speeds


    Additional title:

    J Aeronautical Sciences


    Contributors:

    Published in:

    Publication date :

    1956


    Size :

    11 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :