Global-local model coupling for composite shell structures in the framework of isogeometric analysis

被引:6
作者
Guo, Yujie [1 ,2 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Interdisciplinary Res Inst Aeronaut & Astronaut, Coll Aerosp Engn, Nanjing 210016, Peoples R China
[2] Nanjing Univ Aeronaut & Astronaut, Dept Aircraft Design, Coll Aerosp Engn, Nanjing 210016, Peoples R China
基金
中国国家自然科学基金;
关键词
Isogeometric analysis; Nitsche; Global-local model coupling; Laminate composite shell; Interlaminar stresses; Free edge effects; SHEAR DEFORMATION-THEORY; FINITE CELL METHOD; DIRICHLET BOUNDARY-CONDITIONS; B-REP ANALYSIS; SANDWICH PLATES; FREE-EDGE; LAMINATED COMPOSITE; LAYERWISE THEORY; NITSCHES METHOD; INTERLAMINAR STRESSES;
D O I
10.1016/j.compstruct.2017.05.069
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Nitsche's method had recently demonstrated its potential for a seamless and continuity-preserving coupling of NURBS patches in isogeometric shell analysis. Trimmed and non-conforming patches and even blended models including classical thin-shell and solid-shell formulations can be coupled successfully while preserving a continuous flux along the coupling interfaces. In this paper, we take advantage of the method's modeling flexibility for an extension to NURBS-based laminate composite shell structures. We introduce a global-local model coupling approach to enrich laminate composite thin-shell Kirchhoff-Love models locally with a full three-dimensional continuum solution. The approach provides a reliable coupling of the classical lamina theory with a layerwise formulation revealing the full interlaminar stress state at reduced computational cost. The layerwise shell model is based purely on a mid-surface NURBS description of the shell body thus supporting the direct application of a surface-defined CAD data representation of shells. We apply a refined finite cell approach to handle efficiently trimmed geometries, as common in CAD models. We demonstrate reliability, accuracy of the coupling approach and efficiency in terms of numerical costs and modeling effort of our approach with several examples. (c) 2017 Elsevier Ltd. All rights reserved.
引用
收藏
页码:617 / 629
页数:13
相关论文
共 88 条
[1]   PERFORMANCE OF DIFFERENT INTEGRATION SCHEMES IN FACING DISCONTINUITIES IN THE FINITE CELL METHOD [J].
Abedian, Alireza ;
Parvizian, Jamshid ;
Duester, Alexander ;
Khademyzadeh, Hassan ;
Rank, Ernst .
INTERNATIONAL JOURNAL OF COMPUTATIONAL METHODS, 2013, 10 (03)
[2]  
[Anonymous], 2015, ADV MODEL SIMUL SCI
[3]  
[Anonymous], 1997, NURBS BOOK MONOGRAPH
[4]  
[Anonymous], 2004, ENCYCL COMPUT MECH
[5]   GENERAL 2-DIMENSIONAL THEORY OF LAMINATED CYLINDRICAL-SHELLS [J].
BARBERO, EJ ;
REDDY, JN ;
TEPLY, JL .
AIAA JOURNAL, 1990, 28 (03) :544-553
[6]   Weak imposition of Dirichlet boundary conditions in fluid mechanics [J].
Bazilevs, Y. ;
Hughes, T. J. R. .
COMPUTERS & FLUIDS, 2007, 36 (01) :12-26
[7]   NONLINEAR SHELL FORMULATIONS FOR COMPLETE 3-DIMENSIONAL CONSTITUTIVE LAWS INCLUDING COMPOSITES AND LAMINATES [J].
BRAUN, M ;
BISCHOFF, M ;
RAMM, E .
COMPUTATIONAL MECHANICS, 1994, 15 (01) :1-18
[8]   Analysis in computer aided design: Nonlinear isogeometric B-Rep analysis of shell structures [J].
Breitenberger, M. ;
Apostolatos, A. ;
Philipp, B. ;
Wuechner, R. ;
Bletzinger, K. -U. .
COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING, 2015, 284 :401-457
[9]  
BYRON R, 1970, J COMPOS MATER, V4, P538
[10]   Prediction of in situ strengths and matrix cracking in composites under transverse tension and in-plane shear [J].
Camanho, PP ;
Dávila, CG ;
Pinho, ST ;
Iannucci, L ;
Robinson, P .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2006, 37 (02) :165-176