<P><B>Abstract</B></P> <P>An investigation into the postbuckling and geometrically nonlinear behaviors of functionally graded carbon nanotube-reinforced composite (FG-CNTRC) shells is carried out in this study. The discr...
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https://www.riss.kr/link?id=A107427341
2019
-
SCI,SCIE,SCOPUS
학술저널
983-1003(21쪽)
0
상세조회0
다운로드다국어 초록 (Multilingual Abstract)
<P><B>Abstract</B></P> <P>An investigation into the postbuckling and geometrically nonlinear behaviors of functionally graded carbon nanotube-reinforced composite (FG-CNTRC) shells is carried out in this study. The discr...
<P><B>Abstract</B></P> <P>An investigation into the postbuckling and geometrically nonlinear behaviors of functionally graded carbon nanotube-reinforced composite (FG-CNTRC) shells is carried out in this study. The discrete nonlinear equation system is established based on non-uniform rational B-Spline (NURBS) basis functions and the first-order shear deformation shell theory (FSDT). The nonlinearity of shells is formed in the Total Lagrangian approach considering the von Karman assumption. The incremental solutions are obtained by using a modified Riks method. In the present formulation, the rule of mixture is used to estimate the effective material properties of FG-CNTRC shells. Effects of CNTs distribution, volume fraction and CNTs orientation on the postbuckling behavior of FG-CNTRC shells are particularly investigated. Exact geometries of shells are modeled by using NURBS interpolation. Several verifications are given to show the high reliability of the proposed formulation. Especially, some complex postbuckling curves of FG-CNTRC panels and cylinders are first provided that could be useful for future references.</P> <P><B>Highlights</B></P> <P> <UL> <LI> NURBS-based postbuckling analysis of functionally graded carbon nanotube-reinforced composite shells is performed in this paper. </LI> <LI> The discrete nonlinear equation system is established based on non-uniform rational B-Spline (NURBS) basis functions and the first-order shear deformation shell theory (FSDT). </LI> <LI> The nonlinearity of shells is formed in the Total Lagrangian approach considering the von Karman assumption. </LI> <LI> Effects of CNTs distribution, volume fraction and CNTs orientation on the postbuckling behavior of FG-CNTRC shells are particularly investigated. </LI> <LI> Some complex postbuckling curves of FG-CNTRC panels and cylinders are first provided that could be useful for future references. </LI> </UL> </P>