Failure criteria for use in the design environment

被引:16
作者
Eckold, GC [1 ]
机构
[1] UKAEA, Harwell OX11 0RA, Berks, England
关键词
design environment; process industry; design code;
D O I
10.1016/S0266-3538(96)00144-3
中图分类号
TB33 [复合材料];
学科分类号
摘要
This paper is concerned with the use of composite failure criteria in a design situation. The example chosen is from the process industry which employs composite materials in demanding applications and has requirements for simple, pragmatic and auditable procedures. This is distinct from other environments such as the aerospace industry or in R&D where there are resources available to undertake more sophisticated analyses. In the context of this failure prediction exercise the methods currently adopted by the process sector have been applied, albeit with some modification, since materials of construction are different. Attempts have also been made to predict ultimate strengths, although this is not the prime purpose of a design code, and it is envisaged that there will be some discrepancies owing to the fact that such issues as material non-linearity and differences in tensile and compressive properties are ignored. The more interesting relationship to note will be that between the derived design allowables and the initiation of failure since the basis of chemical process plant design is that normal service loads should be kept within these limits. Crown copyright (C) 1998 Published by Elsevier Science Ltd. All rights reserved.
引用
收藏
页码:1095 / 1105
页数:11
相关论文
共 27 条
[11]   DAMAGE EVOLUTION IN LAMINATED ADVANCED COMPOSITES [J].
JOSHI, SP ;
FRANTZISKONIS, G .
COMPOSITE STRUCTURES, 1991, 17 (02) :127-139
[12]  
McCartney LN, 1994, 142 NPL DMMA
[13]  
NORRIS CB, 1950, 1816 FPL
[14]   STRENGTH OF ANISOTROPIC MATERIALS UNDER COMBINED STRESSES [J].
PUPPO, AH ;
EVENSEN, HA .
AIAA JOURNAL, 1972, 10 (04) :468-&
[15]  
ROBERTS RC, 1978, REINFORCED PLASTICS, P145
[16]  
SMITH TR, 1968, P 6 INT RES PLAST C
[17]   Lamina properties, lay-up configurations and loading conditions for a range of fibre-reinforced composite laminates [J].
Soden, PD ;
Hinton, MJ ;
Kaddour, AS .
COMPOSITES SCIENCE AND TECHNOLOGY, 1998, 58 (07) :1011-1022
[18]   STIFFNESS PROPERTIES OF COMPOSITE LAMINATES WITH MATRIX CRACKING AND INTERIOR DELAMINATION [J].
TALREJA, R .
ENGINEERING FRACTURE MECHANICS, 1986, 25 (5-6) :751-762
[19]  
TOLHOEK P, 1995, COMPOSITE MAT OFFSHO
[20]   GENERAL THEORY OF STRENGTH FOR ANISOTROPIC MATERIALS [J].
TSAI, SW ;
WU, EM .
JOURNAL OF COMPOSITE MATERIALS, 1971, 5 (JAN) :58-+