Flutter Characteristic Study of Composite Sandwich Panel with Functionally Graded Foam Core
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[1] Liviu Librescu,et al. Material grading for improved aeroelastic stability in composite wings , 2007 .
[2] Bifeng Song,et al. Aeroelastic tailoring of composite sandwich panel with lamination parameters , 2016 .
[3] M. Wolcott. Cellular solids: Structure and properties , 1990 .
[4] Hassan Haddadpour,et al. Aero-thermoelastic stability of functionally graded plates , 2007 .
[5] Ermira Junita Abdullah,et al. Structural optimization of an aeroelastically tailored composite flat plate made of woven fiberglass/epoxy , 2008 .
[6] Mohammad Tawfik,et al. Thermal Buckling and Nonlinear Flutter Behavior of Functionally Graded Material Panels , 2007 .
[7] Christine V. Jutte,et al. Aeroelastic tailoring of a plate wing with functionally graded materials , 2014 .
[8] A. Blom,et al. Optimal Design of a Composite Sandwich Structure Using Lamination Parameters , 2012 .
[9] D. Xiao,et al. The influence of correlating material parameters of gradient foam core on free vibration of sandwich panel , 2015 .
[10] Garret N. Vanderplaats,et al. Stiffness Optimization of Orthotropic Laminated Composites Using Lamination Parameters , 1991 .
[11] M. Ganapathi,et al. Asymmetric flexural vibration and thermoelastic stability of FGM circular plates using finite element method , 2006 .
[12] Mohammad Tawfik,et al. Non-linear panel flutter for temperature-dependent functionally graded material panels , 2007 .
[13] James Kennedy,et al. Particle swarm optimization , 2002, Proceedings of ICNN'95 - International Conference on Neural Networks.
[14] Shih-Yao Kuo,et al. Flutter of rectangular composite plates with variable fiber pacing , 2011 .