Flutter behavior of functionally graded graphene origami-reinforced auxetic metamaterial composite laminated plates in supersonic flow
Created by W.Langdon from
gp-bibliography.bib Revision:1.8414
- @Article{XinWang:2025:engstruct,
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author = "Xin Wang and Zhao-Dong Xu and Jun Dai and
Haoyan Peng and Zhenghan Chen and Zhuangzhuang Wang and
Zhiheng Xia and Fengmin Su",
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title = "Flutter behavior of functionally graded graphene
origami-reinforced auxetic metamaterial composite
laminated plates in supersonic flow",
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journal = "Engineering Structures",
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year = "2025",
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volume = "336",
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pages = "120318",
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keywords = "genetic algorithms, genetic programming, Graphene
origami, Flutter analysis, Eigenvalue, FSDT, Modified
Ritz method",
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ISSN = "0141-0296",
-
URL = "
https://www.sciencedirect.com/science/article/pii/S0141029625007096",
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DOI = "
doi:10.1016/j.engstruct.2025.120318",
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abstract = "This paper presents an aeroelastic characteristic of
functionally graded graphene origami-reinforced auxetic
metamaterial (FG-GORAM) composite laminated plates. The
equivalent elastic parameters of each layer, including
elastic modulus, Poisson's ratio, and density, are
determined using the Halpin-Tsai model, modified
through genetic programming (GP) and molecular dynamics
(MD). The artificial boundary springs were introduced
to simulate various boundary constraints, and the
laminated plate's mathematical model was constructed
using the first-order shear deformation theory (FSDT)
coupled with first-order piston theory. The energy
function of the FG-GORAM plate was derived based on
Hamilton's principle, and the solution was obtained
using the modified Ritz method. The accuracy and
validity of the present method were confirmed through
detailed convergence analysis and comparisons with the
published literature data. Furthermore, extensive
parametric analyses were conducted to examine the
effects of boundary conditions, structural parameters
of the plates, and different configurations of graphene
origami. The results indicate that the flutter
performance of FG-GORAM composite laminated plates is
highly dependent on the boundary conditions of the
plate and the different graphene origami
configurations, including their distribution type,
content, and folding degree. It is found that the
FG-GORAM composite plate had better flutter performance
than its plate without the addition of origami
graphene. These findings provide a crucial theoretical
foundation and technological guidance for the design of
such advanced materials",
- }
Genetic Programming entries for
Xin Wang
Zhao-Dong Xu
Jun Dai
Haoyan Peng
Zhenghan Chen
Zhuangzhuang Wang
Zhiheng Xia
Fengmin Su
Citations