An analysis of free vibration of orthogonally stiffened cylindrical shells with stiffeners treated as discrete elements.
Author:
Affiliation:
1. University of Oklahoma, Norman, Okla.
2. NASA Langley Research Center, Hampton, Va.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.4528
Reference26 articles.
1. Circular-Symmetric Vibrations of Infinitely Long Cylindrical Shells With Equidistant Stiffeners
2. Circular Symmetric Vibrations of Ring-Stiffened Cylindrical Shells
3. A SIMPLIFIED MATRIX METHOD FOR THE DYNAMIC EXAMINATION OF DIFFERENT SHELLS OF REVOLUTION
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