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Theory of initially twisted, composite, thin-walled beams
Authors:Wenbin Yu   Lin Liao   Dewey H. Hodges  Vitali V. Volovoi
Affiliation:aDepartment of Mechanical and Aerospace Engineering, Utah State University, Logan, UT 84322-4130, USA;bSchool of Aerospace Engineering, Georgia Institute of Technology, Atlanta, GA 30332-0150, USA
Abstract:
An asymptotically correct theory for initially twisted, thin-walled, composite beams has been constructed by the variational asymptotic method. The strain energy of the original, three-dimensional structure is first rigorously reduced to be a two-dimensional energy expressed in terms of shell strains. Then the two-dimensional strain energy is further reduced to be expressed in terms of the classical beam strain measures. The resulting theory is a classical beam model approximating the three-dimensional energy through the first-order of the initial twist. Consistent use of small parameters that are intrinsic to the problem allows a natural derivation for all thin-walled beams within a common framework, regardless of whether the section is open, closed, or strip-like. Several examples are studied using the present theory and the results are compared with a general cross-sectional analysis, VABS, and other published results.
Keywords:Composite beams   Thin-walled   Initial twist   Asymptotic method   VABS
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