Concept of damping force proportional to amplitude but independent of frequency; experience has indicated that, in structures such as aircraft wings and fuselages, damping loss depends more closely on latter relation; how it compares fundamentally with concept of viscous damping; main points of difference and similarity.


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    Title :

    Note on relations between viscous and structural damping coefficients


    Additional title:

    J Aeronautical Sciences


    Contributors:

    Published in:

    Journal of the Aeronautical Sciences ; 16 , n 7 ; p 409-410 + 448


    Publication date :

    1949


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :





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