Testing at Boeing has progressed from simple half wing cantilever model of 1946 to almost completely scaled flutter models tested in simulation of free flight; continued development of analysis techniques and correlation with full scale flight testing needed for more accurate predictions of flutter characteristics of airplane prior to final design of flight stages.


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    Title :

    Flutter analysis of complex airplanes by experimental methods


    Additional title:

    J Aeronautical Sciences


    Contributors:


    Publication date :

    1952


    Size :

    8 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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