Random response of symmetric cross-ply composite beams with arbitrary boundary conditions
Author:
Affiliation:
1. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.11030
Reference22 articles.
1. Young's and Shear Moduli of Unidirectional Composites by a Resonant Beam Method
2. The Vibration of Cantilever Beams of Fiber Reinforced Material
3. Vibrations of laminated beams
4. An analytic means of determining the flexural and torsional resonant frequencies of generally orthotropic beams
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