An asymptotically correct dynamic shell theory, valid over a wide range of frequencies and wavelengths, is rigorously derived from an analytical point of view. The derivation provides insight and guidance for the numerical modeling of layered shells. This work is based on three essential theoretical foundations: (a) the concept of decomposition of the rotation tensor, which is to establish the dynamic three-dimensional elasticity problem in a compact and elegant intrinsic form for application to the complex geometry of shells; (b) the variational-asymptotic method, which is to perform a systematic and mathematical dimensional reduction in the long-wavelength regime for both low- and high-frequency vibration analysis; and (c) hyperbolic short-wavelength extrapolation, which is to achieve simple, accurate, and positive definite energy functionals for all wavelengths. Based on these, unlike most established shell theories that are limited to the long-wavelength low-frequency regime, the present theory describes in an asymptotically correct manner not only the low-frequency but also some of the first high-frequency branches of vibrations in the long-wave range. Moreover, it recovers the approximate three-dimensional stress state in both long- and short-wavelength ranges.
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January 2009
Research Papers
Dynamic Variational-Asymptotic Procedure for Laminated Composite Shells—Part I: Low-Frequency Vibration Analysis
Chang-Yong Lee, Postdoctoral Fellow,
Chang-Yong Lee, Postdoctoral Fellow
School of Aerospace Engineering,
Georgia Institute of Technology
, Atlanta, GA 30332-0150
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Dewey H. Hodges
Dewey H. Hodges
Professor
Mem. ASME
School of Aerospace Engineering,
Georgia Institute of Technology
, Atlanta, GA 30332-0150
Search for other works by this author on:
Chang-Yong Lee, Postdoctoral Fellow
School of Aerospace Engineering,
Georgia Institute of Technology
, Atlanta, GA 30332-0150
Dewey H. Hodges
Professor
Mem. ASME
School of Aerospace Engineering,
Georgia Institute of Technology
, Atlanta, GA 30332-0150J. Appl. Mech. Jan 2009, 76(1): 011002 (7 pages)
Published Online: October 23, 2008
Article history
Received:
September 5, 2007
Revised:
May 22, 2008
Published:
October 23, 2008
Connected Content
A companion article has been published:
Dynamic Variational-Asymptotic Procedure for Laminated Composite Shells—Part II: High-Frequency Vibration Analysis
Citation
Lee, C., and Hodges, D. H. (October 23, 2008). "Dynamic Variational-Asymptotic Procedure for Laminated Composite Shells—Part I: Low-Frequency Vibration Analysis." ASME. J. Appl. Mech. January 2009; 76(1): 011002. https://doi.org/10.1115/1.3002761
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