Analytical treatment of wing divergence and flutter is in general very involved and often can be carried out only with simplifying assumptions; entirely different method of approach is to build elastically similar model and test it in wind tunnel; brief summary of similarity laws is presented.


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    Title :

    Static and dynamic model similarity


    Additional title:

    J Aeronautical Sciences


    Contributors:
    Nagel, F. (author)

    Published in:

    Publication date :

    1939


    Size :

    2 pages


    Remarks:

    Bibliography


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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