Comments on Nonlinear Vibrations of Immovably Supported Beams by Finite-Element Method
Author:
Affiliation:
1. National Aeronautical Laboratory, Bangalore, India
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.50809
Reference13 articles.
1. Comments on finite element formulation for the large amplitude vibration of tapered beams and beams carrying a concentrated mass
2. Comments on large amplitude vibrations of circular plates
3. Comments on “effect on longitudinal or in-plane deformation and inertia on the large amplitude flexural vibrations of slender beams and thin plates”
4. Comment on "A Finite-Element Approach for Nonlinear Panel Flutter"
5. Comments on the large amplitude asymmetric vibrations of some thin shells of revolution
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