An asymptotically exact methodology, based on geometrically nonlinear, three-dimensional elasticity, is presented for cross-sectional analysis of initially curved and twisted, nonhomogeneous, anisotropic beams. Through accounting for all possible deformation in the three-dimensional representation, the analysis correctly accounts for the complex elastic coupling phenomena in anisotripic beams associated with shear deformation. The analysis is subject only to the restrictions that the strain is small relative to unity and that the maximum dimension of the cross section is small relative to the wave length of the deformation and to the minimum radius of curvature and/or twist. The resulting cross-sectional elastic constants exhibit first-order dependence on the initial curvature and twist. As is well known, the associated geometrically-exact, one-dimensional equilibrium and kinematical equations also depend on initial twist and curvature. Present numerical results show that it is insufficient to account for initial twist and curvature in the beam equations only. The corrections to the stiffness model derived herein are also necessary in general for proper representation of anisotropic beams.
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November 1993
Review Articles
Variational-Asymptotical Analysis of Initially Curved and Twisted Composite Beams
Carlos E. S. Cesnik,
Carlos E. S. Cesnik
School of Aerospace Engineering, Georgia Institute of Technology, Atlanta GA 30332-0150
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Dewey H. Hodges
Dewey H. Hodges
School of Aerospace Engineering, Georgia Institute of Technology, Atlanta GA 30332-0150
Search for other works by this author on:
Carlos E. S. Cesnik
School of Aerospace Engineering, Georgia Institute of Technology, Atlanta GA 30332-0150
Dewey H. Hodges
School of Aerospace Engineering, Georgia Institute of Technology, Atlanta GA 30332-0150
Appl. Mech. Rev. Nov 1993, 46(11S): S211-S220
Published Online: November 1, 1993
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Online:
April 29, 2009
Citation
Cesnik, C. E. S., and Hodges, D. H. (November 1, 1993). "Variational-Asymptotical Analysis of Initially Curved and Twisted Composite Beams." ASME. Appl. Mech. Rev. November 1993; 46(11S): S211–S220. https://doi.org/10.1115/1.3122638
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