Iterative type Rayleigh-Ritz method for natural vibration problems
Author:
Affiliation:
1. Indian Institute of Science, Bangalore, India
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.6011
Reference9 articles.
1. Bisplinghoff, R. L., Holt, A., and Halfman, R. L., Aeroelasticity, Addison-Wesley, Reading, Mass. 1955, pp.136-138, 158-159.
2. The Numerical Treatment of Differential Equations
3. Some Integrals Relating to the Vibration of a Cantilever Beam and Approximation for the Effect of Taper on Overtone Frequencies
4. The Fundamental Flexural Vibration of a Cantilever Beam of Rectangular Cross Section with Uniform Taper
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