Structural Modeling and analysis of composite product system: A graph theoretic approach

被引:14
作者
Prabhakaran, R. T. Durai [1 ]
Babu, B. J. [1 ]
Agrawal, V. P. [1 ]
机构
[1] Birla Inst Technol & Sci, Mech Engn Grp, Zuari Nagar 403726, Goa, India
关键词
composite product system; digraph approach; structural modeling; permanent function;
D O I
10.1177/0021998306061318
中图分类号
TB33 [复合材料];
学科分类号
摘要
An attempt is made to develop an integrated systems model for the structure of the composite product system in terms of its constituents and interactions between the constituents and the molding processes, curing kinetics, etc. using graph theory and matrix algebra. The composite product system is first modeled with the help of a graph theory, then by a variable adjacency matrix and then by a multinomial known as a permanent function. The permanent function provides an opportunity to carry out structural analysis of the composite product in terms of strength, weakness, improvement, and optimization by correlating the properties of a composite with its structure. A physical meaning has been associated with each term of the permanent function. Different structural attributes of the composite product are identified to develop a graph theoretic model, a matrix 6 model, and a multinomial permanent model of the composite. A top-down approach for complete analysis of any composite product system is also given. A general methodology is also presented for characterization and comparison of two composite product systems. Usefulness of the present methodology is also illustrated.
引用
收藏
页码:1987 / 2007
页数:21
相关论文
共 39 条
[1]   The effect of fibre-matrix interactions on structure and property changes during the fabrication of unidirectional carbon/carbon composites [J].
Appleyard, SP ;
Rand, B .
CARBON, 2002, 40 (06) :817-834
[2]   Preliminary study on cost optimisation of aircraft composite structures applicable to liquid moulding technologies [J].
Barlow, D ;
Howe, C ;
Clayton, G ;
Brouwer, S .
COMPOSITE STRUCTURES, 2002, 57 (1-4) :53-57
[3]   The role of sizing resins, coupling agents and their blends on the formation of the interphase in glass fibre composites [J].
Berg, J ;
Jones, FR .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 1998, 29 (9-10) :1261-1272
[4]  
BESSANT B, 2002, REINFORCED PLASTICS, V46, P40
[5]   Influence of reinforcement architecture on damage mechanisms and residual strength of glass-fibre/epoxy composite systems [J].
Bibo, GA ;
Hogg, PJ .
COMPOSITES SCIENCE AND TECHNOLOGY, 1998, 58 (06) :803-813
[6]   The development of a low temperature cure modified epoxy resin system for aerospace composites [J].
Carter, JT ;
Emmerson, GT ;
Lo Faro, C ;
McGrail, PT ;
Moore, DR .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2003, 34 (01) :83-91
[7]   A virtual prototyping system for rapid product development [J].
Choi, SH ;
Chan, AMM .
COMPUTER-AIDED DESIGN, 2004, 36 (05) :401-412
[8]  
Deo N, 2000, GRAPH THEORY APPL EN
[9]  
EDWARDS KL, 1995, MAT DESIGN, V16, P301
[10]   MINERAL POLYMER TOOLING SYSTEM FOR MAKING PROTOTYPE FIBER-REINFORCED COMPOSITE PARTS [J].
FAIGNET, S ;
BAUWERAERTS, P ;
WASTIELS, J ;
WU, X .
JOURNAL OF MATERIALS PROCESSING TECHNOLOGY, 1995, 48 (1-4) :757-764