Time-temperature Dependent Mechanical Properties of Cured Epoxy Resin and Unidirectional CFRP

被引:0
|
作者
Liu, Zhun [1 ]
Guan, Zhidong [1 ]
Liu, Faqi [1 ]
Xu, Jifeng [2 ]
机构
[1] Beihang Univ, Sch Aeronaut Sci & Engn, Beijing, Peoples R China
[2] COMAC, Beijing Aeronaut Sci & Technol Res Inst, Beijing, Peoples R China
来源
2017 8TH INTERNATIONAL CONFERENCE ON MECHANICAL AND AEROSPACE ENGINEERING (ICMAE) | 2017年
关键词
time-temperature dependent; mechanical properties; resin; composite; DOMAIN;
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
For composite structure design, determining the relationships between failure time and mechanical properties in the full range of working temperatures is essential. Dynamic mechanical analysis (DMA) and tensile tests were performed to get the dynamic and static mechanical properties of resin 5228A respectively at various temperatures. The master curves of storage modulus and Young's modulus were constructed at selected reference temperature 25 degrees C using closed form shifting (CFS) method based on the time-temperature superposition principle (TTSP). During the shifting procedure of storage modulus, corresponding time-temperature shift factors were obtained, which meet the Arrhenius equation very well. Finally, the master curves of transverse and longitudinal compressive strength were constructed at 25 degrees C by shifting the compression tests data of unidirectional laminates CCF300/5228A horizontally with the time-temperature shift factors obtained previously. Results show that both dynamic and static mechanical properties of the resin 5228A are obviously time-temperature dependent, higher frequencies induce more elastic-like behavior, transverse and longitudinal compressive strength decreases significantly with increasing failure time.
引用
收藏
页码:113 / 117
页数:5
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