Fatigue life prediction of composites under two-stage loading

被引:19
作者
Otani, N [1 ]
Song, DY [1 ]
机构
[1] UNIV TOKYO,ADV SCI & TECHNOL RES CTR,MEGURO KU,TOKYO 153,JAPAN
关键词
D O I
10.1023/A:1018560423889
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
In order to predict the fatigue life under two-stage loading by formulating a cumulative fatigue damage rule for composite materials, the fatigue process in SiC-Al and glass-fibre reinforced plastics were investigated. A microcrack occurred within the composites which resulted in cumulative fatigue damage that increased linearly with the number of cycles. The mechanical conditions of damage growth and failure were determined by characterizing the microdamage governing the fatigue. The ultimate failure is shown to occur when the product of the stress amplitude ratio and microdamage density is beyond a critical value and an expression for the remaining fatigue life is derived.
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收藏
页码:755 / 760
页数:6
相关论文
共 10 条
[1]  
Broutman L.J., 1972, Compos. Mater.: Test. Des., ASTM STP497, P170
[2]  
BROUTMAN LJ, 1969, P 24 ANN TECHN C WAS
[3]  
FONG JT, 1982, ASTM STP, V775, P243
[4]  
HARRIS B, 1981, AGARD LECT SER, V118
[5]   CUMULATIVE DAMAGE THEORY OF FATIGUE FAILURE [J].
HASHIN, Z ;
ROTEM, A .
MATERIALS SCIENCE AND ENGINEERING, 1978, 34 (02) :147-160
[6]  
KOBAYASHI A, 1985, P 13 S INT COMM AER, P247
[7]  
KOBAYASHI A, 1987, P 14 S INT COMM AER, P195
[8]   PRACTICAL IMPLEMENTATION OF THE DOUBLE LINEAR DAMAGE RULE AND DAMAGE CURVE APPROACH FOR TREATING CUMULATIVE FATIGUE DAMAGE [J].
MANSON, SS ;
HALFORD, GR .
INTERNATIONAL JOURNAL OF FRACTURE, 1981, 17 (02) :169-192
[9]  
MINER MA, 1945, J APPL MECH-T ASME, V12, pA159
[10]  
Reifsnider K.L., 1981, MATERIALS EXPT DESIG, P246