On the modeling and design of composite multilayered structures using solid-shell finite element model
被引:18
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Naceur, H.
[1
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Shiri, S.
论文数: 0引用数: 0
h-index: 0
机构:
Univ Bordeaux 1, Lab I2M, UMR 5295, CNRS,Arts & Metiers ParisTech, F-33607 Pessac, FranceUniv Lille Nord France, Lab LAMIH, UMR8201, CNRS, F-59313 Valenciennes, France
Shiri, S.
[2
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Coutellier, D.
论文数: 0引用数: 0
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机构:
Univ Lille Nord France, Lab LAMIH, UMR8201, CNRS, F-59313 Valenciennes, FranceUniv Lille Nord France, Lab LAMIH, UMR8201, CNRS, F-59313 Valenciennes, France
Coutellier, D.
[1
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Batoz, J. L.
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机构:
Univ Technol Compiegne, Lab Roberval, UMR 6253, CNRS, F-60205 Compigne, FranceUniv Lille Nord France, Lab LAMIH, UMR8201, CNRS, F-59313 Valenciennes, France
Batoz, J. L.
[3
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机构:
[1] Univ Lille Nord France, Lab LAMIH, UMR8201, CNRS, F-59313 Valenciennes, France
[2] Univ Bordeaux 1, Lab I2M, UMR 5295, CNRS,Arts & Metiers ParisTech, F-33607 Pessac, France
[3] Univ Technol Compiegne, Lab Roberval, UMR 6253, CNRS, F-60205 Compigne, France
Composite structures;
Solid-shell;
Optimization;
Design of experiment;
NONLINEAR ANALYSES;
EAS;
D O I:
10.1016/j.finel.2013.02.004
中图分类号:
O29 [应用数学];
学科分类号:
070104 ;
摘要:
In this investigation a coupling between a 3D solid-shell element for the analysis of multilayered composite shell structures and a specific response surface method is proposed. The first part of the paper is dedicated to the finite element formulation of a developed composite 8-node solid-shell element called SCH8 gamma 7, based only on translational degrees of freedom. The basis of the present finite element formulation is the standard 8-node brick element with tri-linear shape functions. A particular attention is given to alleviate shear, trapezoidal and thickness locking, without resorting to the classical plane-stress assumption. Assumed natural strain method and enhanced assumed strain method are used to improve the relative poor element behavior of a standard hexahedral displacement element. The anisotropic material behavior of layered shells is modeled using a fully three dimensional elastic orthotropic material law in each layer, including the thickness stress component. The second part of the paper will focus on an adaptive response surface method for the structural optimization problem. The response surfaces are built using moving least squares approximations and design of experiments by means of a specific method called Diffuse Approximation. Several numerical applications to composite multilayered shell structures are studied to show the applicability and effectiveness of the proposed procedure. Good results of analysis and optimization using the developed SCH8 gamma 7 solid-shell element have been obtained in comparison with reference analytical solutions and with those obtained using the SC8R solid-shell finite element available in ABAQUS(A) code. (C) 2013 Elsevier B.V. All rights reserved.
机构:
Huazhong Univ Sci & Technol, State Key Lab Mat Proc & Die & Mould Technol, Wuhan 430074, Peoples R ChinaHuazhong Univ Sci & Technol, State Key Lab Mat Proc & Die & Mould Technol, Wuhan 430074, Peoples R China
Xu, Heng Jian
Liu, Yu Qi
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Huazhong Univ Sci & Technol, State Key Lab Mat Proc & Die & Mould Technol, Wuhan 430074, Peoples R ChinaHuazhong Univ Sci & Technol, State Key Lab Mat Proc & Die & Mould Technol, Wuhan 430074, Peoples R China
Liu, Yu Qi
Zhang, Zhi Bing
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h-index: 0
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Huazhong Univ Sci & Technol, State Key Lab Mat Proc & Die & Mould Technol, Wuhan 430074, Peoples R ChinaHuazhong Univ Sci & Technol, State Key Lab Mat Proc & Die & Mould Technol, Wuhan 430074, Peoples R China
Zhang, Zhi Bing
Du, Ting
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Huazhong Univ Sci & Technol, State Key Lab Mat Proc & Die & Mould Technol, Wuhan 430074, Peoples R ChinaHuazhong Univ Sci & Technol, State Key Lab Mat Proc & Die & Mould Technol, Wuhan 430074, Peoples R China
机构:
Univ Politecn Cataluna, Jordi Girona 1-3,Edif C1, Barcelona 08034, Spain
Univ Santiago Chile, Av Libertador Bernardo OHiggins 3363,Estn Cent, Santiago, ChileUniv Politecn Cataluna, Jordi Girona 1-3,Edif C1, Barcelona 08034, Spain
Aguirre, A.
Codina, R.
论文数: 0引用数: 0
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Univ Politecn Cataluna, Jordi Girona 1-3,Edif C1, Barcelona 08034, Spain
Ctr Int Metodes Numer Engn CIMNE, Gran Capita S N,Edif C1, Barcelona 08034, SpainUniv Politecn Cataluna, Jordi Girona 1-3,Edif C1, Barcelona 08034, Spain
Codina, R.
Baiges, J.
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h-index: 0
机构:
Univ Politecn Cataluna, Jordi Girona 1-3,Edif C1, Barcelona 08034, Spain
Ctr Int Metodes Numer Engn CIMNE, Gran Capita S N,Edif C1, Barcelona 08034, SpainUniv Politecn Cataluna, Jordi Girona 1-3,Edif C1, Barcelona 08034, Spain
Baiges, J.
Castanar, I.
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Univ Politecn Cataluna, Jordi Girona 1-3,Edif C1, Barcelona 08034, SpainUniv Politecn Cataluna, Jordi Girona 1-3,Edif C1, Barcelona 08034, Spain
机构:
School of Aeronautics, Northwestern Polytechnical University, Xi'an,710072, China
National Key Laboratory of Aircraft Configuration Design, Xi'an,710072, ChinaSchool of Aeronautics, Northwestern Polytechnical University, Xi'an,710072, China
Liang, Ke
Hao, Qiuyang
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机构:
School of Aeronautics, Northwestern Polytechnical University, Xi'an,710072, ChinaSchool of Aeronautics, Northwestern Polytechnical University, Xi'an,710072, China
Hao, Qiuyang
Li, Zheng
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School of Aeronautics, Northwestern Polytechnical University, Xi'an,710072, ChinaSchool of Aeronautics, Northwestern Polytechnical University, Xi'an,710072, China
Li, Zheng
Cheng, Qian
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School of Aeronautics, Northwestern Polytechnical University, Xi'an,710072, ChinaSchool of Aeronautics, Northwestern Polytechnical University, Xi'an,710072, China
机构:
Ho Chi Minh City Univ Technol HUTECH, CIRTech Inst, Ho Chi Minh City, Vietnam
Sejong Univ, Dept Architectural Engn, 209 Neungdong Ro, Seoul 05006, South KoreaUniv Calabria, Dipartimento Ingn Informat Modellist Elettron & S, I-87036 Cosenza, Italy