Postcuring effects on impact behavior of glass/epoxy composite laminates

被引:5
|
作者
Kumar, CR
Radhakrishna, K
Rao, RMVGK [1 ]
机构
[1] Natl Aeronaut Labs, Fibre Reinforced Plast Div, Bangalore 560017, Karnataka, India
[2] BMS Coll Engn, Bangalore, Karnataka, India
关键词
glass/epoxy composite; postcure; impact behavior; glass transition temperature;
D O I
10.1177/0731684405048194
中图分类号
TB33 [复合材料];
学科分类号
摘要
Studies had been undertaken on the effects of different postcure schedules on the impact resistance of RT-cured glass/epoxy laminates, subjected to repeated drop tests using an in-house built uninstrumented drop weight impact tester. The impact resistance was assessed in terms of two parameters, viz., the number of drops to failure (N-f) and the delamination area growth (dA). The specimens were postcured at different time-temperature combinations and the impact response was studied at three different incident energy levels (10.6, 12.6, and 14.8J). It was found that, the Nf and dA values increased to a maximum at an optimum postcure schedule of 85 degrees C/4 h. The extent of composite cure for the different postcure schedules was ascertained by measuring the glass transition temperatures (T-g), in order to obtain an appreciation for correlation between the impact resistance and the chemical cure status of the composite. Also, single drop impact studies were made at the 25-J energy level using an instrumented impact tester (DYNATUP 8250) and the aforesaid optimum postcure schedule was reconfirmed.
引用
收藏
页码:949 / 960
页数:12
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