Variational finite element-tensor formulation for the large deflection random vibration of composite plates
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1991-1240
Reference10 articles.
1. Sonic fatigue and nonlinear response of stiffened panels
2. Development of an implicit method with numerical dissipation from a generalized single-step algorithm for structural dynamics
3. A finite element formulation for the large deflection random response of thermally buckled plates
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