Effect of Mode Shape Switching on the Loss Factor of Sandwich Cylinders
Author:
Affiliation:
1. Sharif University of Technology, 11155-8639 Tehran, Iran
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference60 articles.
1. Damping of Flexural Waves by a Constrained Viscoelastic Layer
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4. Forced vibrations of damped cylindrical shells filled with pressurized liquid
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