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.
Note on relations between viscous and structural damping coefficients
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 16 , n 7 ; p 409-410 + 448
1949
Aufsatz (Zeitschrift)
Englisch
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