Publication: Vibration and Damping Analysis of Sandwich Cylindrical Shells by the GDQM
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American Institute of Aeronautics and Astronautics (AIAA)
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This paper focuses on the vibration and damping analysis of three-layered sandwich cylindrical shells with stiff composite face layers and a viscoelastic core. The equations of motion and boundary ...
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AIAA Journal
ISSN
0001-1452
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