A study of factors affecting life prediction of composites under spectrum loading

被引:43
作者
Passipoularidis, V. A. [1 ]
Philippidis, T. P. [1 ]
机构
[1] Univ Patras, Dept Aeronaut & Mech Engn, Patras 26504, Greece
关键词
Composites; Spectrum fatigue; Damage accumulation rule; Constant life diagram; RESIDUAL STRENGTH; FATIGUE; METHODOLOGY; MODEL;
D O I
10.1016/j.ijfatigue.2008.07.010
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The influence of damage accumulation metric, constant life diagram formulation and cycle counting method on life prediction schemes for composite materials under variable amplitude (VA) loading is investigated in this paper. Special focus is put on residual strength based methodologies; different degradation functions are implemented and compared with the Palmgren-Miner (PM) damage accumulation rule, The predictions are validated by comparison with experimental data from a unidirectional glass/ epoxy laminate cycled with three different loading spectra. The effect of constant life diagram (CLD) and cycle counting method used in life prediction is investigated through implementation of alternative existing formulations. Results indicate that a net improvement is achieved when linear strength degradation is implemented as damage metric in life prediction schemes, over the state-of-the-art PM summation. Depending on the spectrum pattern itself, CLD and counting method might be of predominant role; Rainflow counting and the simplistic concept according to which a single S-N curve describes fatigue response of the material under any loading condition (R ratio) are shown to yield consistently best life predictions. (C) 2008 Elsevier Ltd. All rights reserved.
引用
收藏
页码:408 / 417
页数:10
相关论文
共 37 条
[1]   A POWER LAW FATIGUE DAMAGE MODEL FOR FIBER-REINFORCED PLASTIC LAMINATES [J].
ADAM, T ;
DICKSON, RF ;
JONES, CJ ;
REITER, H ;
HARRIS, B .
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART C-JOURNAL OF MECHANICAL ENGINEERING SCIENCE, 1986, 200 (03) :155-166
[2]  
Adams B.M., 1994, Quality Engineering, V6, P533
[3]  
[Anonymous], OBTG5R013
[4]  
[Anonymous], 2003, FATIGUE COMPOSITES
[5]  
[Anonymous], 1979, FRACT MECH, DOI DOI 10.1016/B978-0-08-024766-3.50009-4
[6]  
[Anonymous], P SPEC TOP C CREAT T
[7]  
[Anonymous], 1982, PROG SCI ENG COMPOS
[8]  
[Anonymous], P 18 RIS INT S MAT S
[9]  
ASTM, ASTM E1049-85
[10]   Fatigue life prediction for GRP subjected to variable amplitude loading [J].
Bond, IP .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 1999, 30 (08) :961-970