回顾了纤维复合材料在疲劳加载下的剩余强度的描述方法和试验结果,并按照纤维复合材料中疲劳损伤发展的行为,提出了一个描述纤维复合材料的剩余强度的模型,该模型考虑了疲劳损伤在纤维复合材料中产生和扩展的特征,试验结果与理论描述吻合较好.
参考文献
[1] | Talreja R. Fatigue of composite materials. Technomic Publishing Co, Inc, 1987. 181p |
[2] | Broutman L J, Sahu S. A new theory to predict cumulative fatigue damage in fibre-glass reinforced plastics. Composite Materials: Testing and Design(2nd Conference), ASTM STP497, 1972. 170~188 |
[3] | Yang J N, Jones D L. Load sequence on the fatigue of unnotched composite materials. Fatigue of Fibrous Composite Materials, ASTM STP 723, 1981. 213~232 |
[4] | Hashin Z. Cumulative damage theory for composite materials: residual life and residual strength methods. Composites Science and Technology, 1985, 23:1~19 |
[5] | Hahn T. Fatigue behaviour and life prediction of composite laminates, AFML-TR-78-43, 1978 |
[6] | Chou P C, Croman R. Residual strength in fatigue based on the strength-life equal rank assumption. Journal of Composite Materials, 1978, 12:177~194 |
[7] | Chou P C, Croman R. Degradation and sudden-death models of fatigue of graphite/epoxy composites. In: Composite Materials: Testing and Design (Fifth Conference), ASTM STP 674, 1979. 431~454 |
[8] | Charewicz A, Daniel I M. Damage mechanisms and accumulation in graphite/epoxy laminates. In: Composite Materials: Fatigue and Fracture (Hahn H T, Ed), ASTM STP 907, 1986. 274~297 |
[9] | Schaff J R, Davidson B D. Life prediction methodology for composite structures. Part I-Constant amplitude and two-stress level fatigue. Journal of Composite Materials, 1997, 31:128~157 |
[10] | Donaldson S L, Kim R Y. Life prediction of glass/vinylester and glass/polyerster composites under fatigue loading, Proceedings of ICCM-10, 1995. I577~I584 |
[11] | Yang J N, Liu M D. Residual strength degradation model and theory of periodic proof tests for graphite/epoxy laminates. AFML-TR-76-225, Wright-Patterson AFB, 1976 |
[12] | Ryder J T, Walker E K. Ascertainment of the effect of compressive loading on the fatigue lifetime of graphite epoxy laminates for structural application. AFML-TR-76-241, Wright-Patterson AFB, 1976 |
[13] | Tai N H, Ma C C M, Wu S H. Fatigue behaviour of carbon fibre/PEEK laminate composites. Composites, 1995, 26(8): 551~559 |
上一张
下一张
上一张
下一张
计量
- 下载量()
- 访问量()
文章评分
- 您的评分:
-
10%
-
20%
-
30%
-
40%
-
50%