A GENERAL STRENGTH THEORY FOR COMPOSITE-MATERIALS BASED ON DUAL KRIGING INTERPOLATION

被引:9
作者
ECHAABI, J [1 ]
TROCHU, F [1 ]
GAUVIN, R [1 ]
机构
[1] ECOLE POLYTECH,MONTREAL,PQ H3C 3A7,CANADA
关键词
COMPOSITE MATERIALS; FAILURE ENVELOPE; KRIGING; GRAPHITE-EPOXY; PAPERBOARD;
D O I
10.1177/073168449501400302
中图分类号
TB33 [复合材料];
学科分类号
摘要
Failure behaviour of composite materials presents several characteristics which depend on the materials selected, the manufacturing process used and the state of stress or strain. An important number of strength criteria have been applied to model failure in the last two decades. Each criterion is different and can be used to fit particular experimental results. Up to now, there is no general and systematic approach to describe the failure of composite materials. In this study, a general strength theory based on dual kriging is proposed to model the failure behaviour of composite materials. The theoretical background of the method is first presented, then its application to model failure of composite materials is demonstrated on two examples: a graphite-epoxy composite and paperboard. The mathematical expression of the criterion can be obtained either through a parametric or an implicit formulation. The parametric formulation is used to predict three-dimensional failure envelopes of graphite-epoxy fabrics and paperboard. The method shows an excellent agreement with available experimental data. Different types of interpolating functions, can be used such as polynomials or trigonometric functions. The results obtained are compared with the tenser quadratic, tenser cubic and parametric criteria. The model can be improved when a nugget effect is added in the kriging equations: the interpolating function does no longer fit the data points. This approach permits incorporating the effect of measurements errors in the interpolation procedure. The intensity of the nugget effect is usually chosen to be proportional to the variance error. The uncertainty of the measurements is thus reflected on the shape of the failure envelope. Note that general tenser polynomial criteria can be derived as a limit case of this approach, and additional experimental data incorporated in the model to refine its accuracy. The proposed methodology can be used as a general and systematic tool to model effectively a great variety of failure behaviours.
引用
收藏
页码:211 / 232
页数:22
相关论文
共 20 条
[1]  
BRODLIE KW, 1985, NATO ASI SERIES F, V17
[2]  
GILBERT R, 1990, J APPLICATIONS ADV I, V2
[3]  
Gol'denblat II., 1965, MEKH POLIM, V1, P54, DOI 10.1007/BF00860685
[4]  
JIANG Z, 1989, J COMP MATE, V23
[5]  
JOURNEL AG, 1978, HUIJBREGTS
[6]  
Krige DG, 1951, J S AFR I MIN METALL, V52, P119
[7]  
LABOSSIERE P, 1988, POLYM COMPOSITES, V9
[8]  
MAKINDE A, 1992, POLYM COMPOSITES, V13
[9]  
Matheron G., 1973, Advances in Applied Probability, V5, P439, DOI 10.2307/1425829
[10]  
Nahas M. N., 1986, Journal of Composites Technology and Research, V8, P138, DOI 10.1520/CTR10335J