Methods for determination of dynamic stability derivates of aircraft are grouped into test objects free to move in all basic degrees of freedom and test objects rigidly restricted in several basic degrees; to first group belong full scale and free flight model tests; model tests in aeroballistics range and free flight model tests in wind tunnel; second group deals with models moving in test section and fixed models; basic aspects of each method.


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    Title :

    Methods of measurement of aircraft dynamic stability derivatives


    Additional title:

    Can Aeronautical J


    Contributors:

    Published in:

    Publication date :

    1960


    Size :

    9 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :




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