A new cumulative fatigue damage model for fibre-reinforced plastics

被引:139
作者
Yao, WX
Himmel, N [1 ]
机构
[1] Univ Kaiserslautern, Inst Composite Mat Ltd, D-67663 Kaiserslautern, Germany
[2] Nanjing Univ Aeronaut & Astronaut, Dept Aircraft Engn, Nanjing 210016, Peoples R China
关键词
cumulative fatigue damage model; P-M rule; residual strength; FRP; variable amplitude loading;
D O I
10.1016/S0266-3538(99)00100-1
中图分类号
TB33 [复合材料];
学科分类号
摘要
A cumulative fatigue damage model is presented for predicting the fatigue life of fibre-reinforced plastics (FRP) subjected to variable amplitude fatigue loading. It is assumed that the cumulative fatigue damage caused by the cyclic loading is proportional to the strength loss of FRP, and that the damage state in laminates can be described phenomenologically by residual strength. Some experimental results from two-stress level and block spectrums are employed to evaluate the model. Good coincidence between experiment and theory has been obtained for GRP and CFRP. (C) 2000 Elsevier Science Ltd. All rights reserved.
引用
收藏
页码:59 / 64
页数:6
相关论文
共 29 条
[1]   LIFE PREDICTION FOR FATIGUE OF T800/5245 CARBON-FIBER COMPOSITES .2. VARIABLE-AMPLITUDE LOADING [J].
ADAM, T ;
GATHERCOLE, N ;
REITER, H ;
HARRIS, B .
INTERNATIONAL JOURNAL OF FATIGUE, 1994, 16 (08) :533-547
[2]  
ANDERSONS J, 1997, P ICCM 11
[3]  
[Anonymous], 1987, FATIGUE COMPOSITE MA
[4]  
Broutman L.J., 1972, Compos. Mater.: Test. Des., ASTM STP497, P170
[5]  
CHAREWICZ A, 1986, ASTM STP, V907, P274, DOI DOI 10.1520/STP19991S
[6]  
CHOU PC, 1978, J COMPOS MATER, V12, P177
[7]  
DONALDSON SL, 1995, P ICCM 10, P1577
[8]   PROOF TESTING OF COMPOSITE-MATERIALS [J].
HAHN, HT ;
KIM, RY .
JOURNAL OF COMPOSITE MATERIALS, 1975, 9 (JUL) :297-311
[9]   FATIGUE BEHAVIOR OF COMPOSITE LAMINATE [J].
HAHN, HT ;
KIM, RY .
JOURNAL OF COMPOSITE MATERIALS, 1976, 10 (APR) :156-180
[10]  
HAHN HT, 1982, ASTM STP, V787, P247