Lowest Twelve Frequencies of Sandwich Plates Using Third-Order Shear-Normal Deformation Theory
Author:
Affiliation:
1. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24060
Funder
Office of Naval Research
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.J058920
Reference36 articles.
1. An overview of layerwise theories for composite laminates and structures: Development, numerical implementation and application
2. CZ° requirements—models for the two dimensional analysis of multilayered structures
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5. An unsymmetric FRC laminate C° finite element model with 12 degrees of freedom per node
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