The role of shear deformation in laminated plates with curvilinear fiber paths and embedded defects

被引:43
作者
Akbarzadeh, A. H. [1 ]
Nik, M. Arian [1 ]
Pasini, D. [1 ]
机构
[1] McGill Univ, Dept Mech Engn, Montreal, PQ H3A 0C3, Canada
关键词
Automated Fiber Placement; Fourier-Galerkin method; Gaps and overlaps; Moderately-thick laminated composite; Variable stiffness laminates; EQUIVALENT-SINGLE-LAYER; STIFFNESS COMPOSITE PANELS; FREE-VIBRATION ANALYSIS; DIFFERENTIAL QUADRATURE; TRANSVERSE-SHEAR; STATIC ANALYSIS; BUCKLING ANALYSIS; DYNAMIC-ANALYSIS; SANDWICH; DESIGN;
D O I
10.1016/j.compstruct.2014.07.027
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Automated Fiber Placement (AFP) is an advanced technology used to manufacture laminated composites with curvilinear fiber paths. During the manufacturing, AFP generally leads to the formation of defects, e.g. gaps and overlaps, that impact the laminate properties, to an extent that largely depends on the geometry, such as thickness and curvature, of the part. This paper focuses on moderately-thick laminate plates that present gaps and overlaps induced by AFP. We use higher-order shear deformation theories to study the role of shear deformation on the plate responses. A hybrid Fourier-Galerkin method is used to obtain a semi-analytic solution describing the static deformation of the plate. Eigenvalue analysis is also conducted to determine its fundamental frequency and critical buckling load. The numeric results show that shear deformation has a more severe impact on the structural responses of a variable stiffness than a constant stiffness plate. We find also that gaps deteriorate the structural performance, while overlaps improve it. Maps representing structural responses, in particular buckling vs. deflection and frequency vs. deflection, are generated to gain insight into the design of a variable stiffness laminate plate with defects. (C) 2014 Elsevier Ltd. All rights reserved.
引用
收藏
页码:217 / 227
页数:11
相关论文
共 62 条
[21]   Postbuckling analysis of laminated composite plates subjected to the combination of in-plane shear, compression and lateral loading [J].
Han, Sung-Cheon ;
Lee, Sang-Youl ;
Rus, Guillermo .
INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 2006, 43 (18-19) :5713-5735
[22]   Natural frequencies and vibration modes of laminated composite plates reinforced with arbitrary curvilinear fiber shape paths [J].
Honda, Shinya ;
Narita, Yoshihiro .
JOURNAL OF SOUND AND VIBRATION, 2012, 331 (01) :180-191
[23]   Vibration design of laminated fibrous composite plates with local anisotropy induced by short fibers and curvilinear fibers [J].
Honda, Shinya ;
Narita, Yoshihiro .
COMPOSITE STRUCTURES, 2011, 93 (02) :902-910
[24]   Nonlinear vibration and dynamic response of shear deformable laminated plates in hygrothermal environments [J].
Huang, XL ;
Shen, HS ;
Zheng, JJ .
COMPOSITES SCIENCE AND TECHNOLOGY, 2004, 64 (10-11) :1419-1435
[25]   Analytical solutions for free vibration of laminated composite and sandwich plates based on a higher-order refined theory [J].
Kant, T ;
Swaminathan, K .
COMPOSITE STRUCTURES, 2001, 53 (01) :73-85
[26]   Static and dynamic analysis of an FGM doubly curved panel resting on the Pasternak-type elastic foundation [J].
Kiani, Y. ;
Akbarzadeh, A. H. ;
Chen, Z. T. ;
Eslami, M. R. .
COMPOSITE STRUCTURES, 2012, 94 (08) :2474-2484
[27]   Static Analysis of Functionally Graded Piezoelectric Beams under Thermo-Electro-Mechanical Loads [J].
Komeili, Amin ;
Akbarzadeh, Abdol Hamid ;
Doroushi, Arezou ;
Eslami, Andmohammad Reza .
ADVANCES IN MECHANICAL ENGINEERING, 2011,
[28]   Buckling analysis of laminated composite plates containing delaminations using the enhanced assumed strain solid element [J].
Lee, Sang-Youl ;
Park, Dae-Yong .
INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 2007, 44 (24) :8006-8027
[29]   Finite element dynamic stability analysis of laminated composite skew plates containing cutouts based on HSDT [J].
Lee, Sang-Youl .
COMPOSITES SCIENCE AND TECHNOLOGY, 2010, 70 (08) :1249-1257
[30]   Free and forced vibration analysis of laminated composite plates and shells using a 9-node assumed strain shell element [J].
Lee, Won-Hong ;
Han, Sung-Cheon .
COMPUTATIONAL MECHANICS, 2006, 39 (01) :41-58