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Finite element analysis of laminated composite shell junctions
Authors:H.V. Lakshminarayana
Affiliation:National Aeronautical Laboratory, Bangalore-560017, India
Abstract:The axisymmetric bending of laminated composite shell junctions have been analysed by the finite element displacement method using laminated anisotropic shell theory. Numerical results have been presented for cylinder-cone shell junction and cylinder-geodesic-isotensoid dome junction. These results have been compared with results for isotropic case.
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