Investigation of supersonic flutter of thick doubly curved sandwich panels with \CNT\ reinforced facesheets using higher-order structural theory

Abstract : In this paper, the supersonic flutter characteristics of doubly curved sandwich shell panels, viz., cylindrical and spherical shells, with carbon nanotube (CNT) reinforced facesheets are investigated using QUAD-8 shear flexible shell element developed based on higher-order structural theory. The formulation accounts for the nonlinear variation of the in-plane and transverse displacements through the thickness, and abrupt discontinuity in slope of the in-plane displacement at the interface. The strain–displacement relation is accurately introduced in the formulation. The first-order high Mach number approximation to linear potential flow theory is employed for evaluating the aerodynamic pressure. The solutions of the complex eigenvalue problem, developed based on Lagrange’s equation of motion, are obtained by \QR\ algorithm. The accuracy of the present formulation is validated considering the problems for which solutions are available in the literature. A detailed numerical study is conducted to highlight the significance of the higher-order model over the first-order theory and also to examine the influence of the volume fraction of the CNT, core-to-face sheet thickness, the shell thickness and the aspect ratio, radius-to-thickness ratio, and temperature on the flutter boundaries.
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Article dans une revue
Composite Structures, Elsevier, 2015, 127, pp.340 - 355. 〈10.1016/j.compstruct.2015.02.047〉
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https://hal.univ-lorraine.fr/hal-01417907
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Soumis le : vendredi 16 décembre 2016 - 10:53:29
Dernière modification le : jeudi 19 avril 2018 - 15:36:07

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A. Sankar, S. Natarajan, Tarak Ben Zineb, M. Ganapathi. Investigation of supersonic flutter of thick doubly curved sandwich panels with \CNT\ reinforced facesheets using higher-order structural theory. Composite Structures, Elsevier, 2015, 127, pp.340 - 355. 〈10.1016/j.compstruct.2015.02.047〉. 〈hal-01417907〉

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