A general approach forcing convexity of ply angle optimization in composite laminates

被引:0
|
作者
J. Foldager
J. S. Hansen
N. Olhoff
机构
[1] Aalborg University,Institute of Mechanical Engineering
[2] University of Toronto,Institute for Aerospace Studies
[3] Aalborg University,Institute of Mechanical Engineering
来源
Structural optimization | 1998年 / 16卷
关键词
Design Variable; Design Space; Composite Structure; Composite Laminate; Major Shortcoming;
D O I
暂无
中图分类号
学科分类号
摘要
This paper deals with optimization of laminated composite structures in which the ply angles are taken as design variables. One of the major problems when using ply-angles as design variables, is the lack of convexity of the objective function and thus the existence of local optima, which implies that usual gradient based optimization procedures may not be effective. Therefore, a new general approach that avoids the abovementioned problems of nonconvexity when ply-angles are used as design variables is proposed. The methodology is based upon the fact that the design space for an optimization problem formulated in lamination parameters [introduced by Tsai and Pagano (1968)] is proven to be convex, because the laminate stiffnesses are expressed linearly in terms of the lamination parameters. However, lamination parameters have at least two major shortcomings: as yet, for the general case involving membrane-bending coupling, the constraints between the lamination parameters are not completely defined; also, for a prescribed set of lamination parameters physically realizable composite laminates (e.g. laminates with equal thickness plies) may not exist. The approach here, uses both lamination parameters and ply-angles and thereby uses the advantages of both and eliminates the shortcomings of both.
引用
收藏
页码:201 / 211
页数:10
相关论文
共 50 条
  • [41] A synergistic damage mechanics approach to mechanical response of composite laminates with ply cracks
    Singh, Chandra Veer
    Talreja, Ramesh
    JOURNAL OF COMPOSITE MATERIALS, 2013, 47 (20-21) : 2475 - 2502
  • [42] Ply angle optimization of nonuniform composite beams subject to aeroelastic constraints
    Evrard, T
    Butler, R
    Hughes, SW
    Banerjee, JR
    AIAA JOURNAL, 2000, 38 (10) : 1992 - 1994
  • [43] Derived Dynamic Ply Properties from Test Data on Angle Ply Laminates
    F. A. R. Al-Salehi
    S. T. S. Al Hassani
    N. M. Bastaki
    M. J. Hinton
    Applied Composite Materials, 1997, 4 : 157 - 172
  • [44] Finite element analysis of transverse cracking behaviour in hybrid angle-ply composite laminates
    Pradhan, B
    Kumar, NV
    Rao, NS
    JOURNAL OF REINFORCED PLASTICS AND COMPOSITES, 1999, 18 (15) : 1428 - 1448
  • [45] Derived dynamic ply properties from test data on angle ply laminates
    Univ of Manchester Inst of Science, and Technology, Manchester, United Kingdom
    Appl Compos Mater, 3 (157-172):
  • [46] ANALYTICAL INVESTIGATION ON BUCKLING STABILITY OF GLASS/CARBON HYBRID ANGLE-PLY COMPOSITE LAMINATES
    Adim, Belkacem
    Hassaine Daouadji, Tahar
    ACTA TECHNICA NAPOCENSIS SERIES-APPLIED MATHEMATICS MECHANICS AND ENGINEERING, 2022, 65 (02): : 147 - 154
  • [47] The effect of fibre alignment on composite strength .2. The strength of angle-ply laminates
    Khatibzadeh, M
    Piggott, MR
    COMPOSITES SCIENCE AND TECHNOLOGY, 1996, 56 (12) : 1443 - 1451
  • [48] Derived dynamic ply properties from test data on angle ply laminates
    AlSalehi, FAR
    AlHassani, STS
    Bastaki, NM
    Hinton, MJ
    APPLIED COMPOSITE MATERIALS, 1997, 4 (03) : 157 - 172
  • [49] A micromechanics based predictive model for damage initiation in compressively loaded angle ply composite laminates
    Ahn, J
    Waas, AM
    COLLECTION OF THE 41ST AIAA/ASME/ASCE/AHS/ASC STRUCTURES, STRUCTURAL DYNAMICS, AND MATERIALS CONFERENCE AND EXHIBIT, VOL 1 PTS 1-3, 2000, : 2048 - 2057
  • [50] Effect of Off – Axis Matrix Cracking on Stiffness of Symmetric Angle-Ply Composite Laminates
    D. G. Katerelos
    L. N. McCartney
    C. Galiotis
    International Journal of Fracture, 2006, 139 : 529 - 536