Energy based collocation method to predict progressive damage behavior of imperfect composite plates under compression

被引:15
作者
Ghannadpour, S. A. M. [1 ]
Shakeri, M. [1 ]
机构
[1] Shahid Beheshti Univ, GC, New Technol & Engn Dept, Tehran, Iran
来源
LATIN AMERICAN JOURNAL OF SOLIDS AND STRUCTURES | 2018年 / 15卷 / 04期
关键词
Progressive damage; Hashin failure criterion; Collocation; Composite plate; Legendre-Gauss-Lobatto nodes; Initial imperfection; GEOMETRIC NONLINEAR-ANALYSIS; BUCKLING STRENGTH ANALYSIS; FINITE STRIP; LAMINATED PLATES; POSTBUCKLING ANALYSIS; INITIAL IMPERFECTION; STIFFENED PLATES; LARGE-DEFLECTION; VERSIONS;
D O I
10.1590/1679-78254257
中图分类号
TU [建筑科学];
学科分类号
0813 ;
摘要
A new collocation methodology is presented to predict failure and progressive damage behavior of composite plates in this paper. The present work deals with composite plates containing initial geometric imperfections and different boundary conditions under uniaxial in-plane compressive load. In the present study, the domain is discretized with Legendre-Gauss-Lobatto nodes and the approximation of displacement fields is performed by Legendre Basis Functions (LBF5). The onset of damage and damage evolution are predicted by Hashin's failure criteria and by proposed material degradation models. Three geometric degradation models are also assumed to estimate the degradation zone around the failure location which are named complete, region and node degradation models.
引用
收藏
页数:25
相关论文
共 47 条
  • [11] Carrera Erasmo, 2013, 9 INT S VIBR CONT SY
  • [12] CHEUNG YK, 1976, FINITE STRIP METHOD, P26
  • [13] ON THE THEORY OF LAMINATED ANISOTROPIC SHELLS AND PLATES
    DONG, SB
    PISTER, KS
    TAYLOR, RL
    [J]. JOURNAL OF THE AEROSPACE SCIENCES, 1962, 29 (08): : 969 - 975
  • [14] A high order collocation method for the static and vibration analysis of composite plates using a first-order theory
    Ferreira, A. J. M.
    Castro, Luis M. S.
    Bertoluzza, Silvia
    [J]. COMPOSITE STRUCTURES, 2009, 89 (03) : 424 - 432
  • [15] An exact finite strip for the calculation of relative post-buckling stiffness of I-section struts
    Ghannadpour, S. A. M.
    Ovesy, H. R.
    [J]. INTERNATIONAL JOURNAL OF MECHANICAL SCIENCES, 2008, 50 (09) : 1354 - 1364
  • [16] Pseudo spectral method in nonlinear analysis of relatively thick imperfect laminated plates under end-shortening strain
    Ghannadpour, S. A. M.
    Kiani, P.
    Reddy, J. N.
    [J]. COMPOSITE STRUCTURES, 2017, 182 : 694 - 710
  • [17] Initial imperfection effects on postbuckling response of laminated plates under end-shortening strain using Chebyshev techniques
    Ghannadpour, S. A. M.
    Barekati, M.
    [J]. THIN-WALLED STRUCTURES, 2016, 106 : 484 - 494
  • [18] FATIGUE FAILURE CRITERION FOR FIBER REINFORCED MATERIALS
    HASHIN, Z
    ROTEM, A
    [J]. JOURNAL OF COMPOSITE MATERIALS, 1973, 7 (OCT) : 448 - 464
  • [19] Studies of the buckling of composite plates in compression
    Hayman, B.
    Berggreen, C.
    Lundsgaard-Larsen, C.
    Delarche, A.
    Toftegaard, H.
    Dow, R. S.
    Downes, J.
    Misirlis, K.
    Tsouvalis, N.
    Douka, C.
    [J]. SHIPS AND OFFSHORE STRUCTURES, 2011, 6 (1-2) : 81 - 92
  • [20] Krysl P, 1995, COMPUT MECH, V17, P26