Temperature Effects on Mechanical Properties of Woven Thermoplastic Composites for Secondary Aircraft Structure Applications
The effect of temperature on the mechanical behavior of 8-H satin woven glass fabric/polyethylene sulfide (GF/PPS) was investigated in this paper. Static-tensile tests were both conducted on notched and unnotched specimens at typical temperatures (ambient, 95°C and 125°C) based on the glass transiti...
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2017-01-01
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Series: | MATEC Web of Conferences |
Online Access: | https://doi.org/10.1051/matecconf/201710801009 |
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doaj-d2bced74c4824d14a7e4c37c440af5d82021-02-02T00:49:27ZengEDP SciencesMATEC Web of Conferences2261-236X2017-01-011080100910.1051/matecconf/201710801009matecconf_icmaa2017_01009Temperature Effects on Mechanical Properties of Woven Thermoplastic Composites for Secondary Aircraft Structure ApplicationsWang YueZhang JipengZhang JiazhenZhou ZhengongThe effect of temperature on the mechanical behavior of 8-H satin woven glass fabric/polyethylene sulfide (GF/PPS) was investigated in this paper. Static-tensile tests were both conducted on notched and unnotched specimens at typical temperatures (ambient, 95°C and 125°C) based on the glass transition temperatures (Tg) of the neat resin and composite, their strength and moduli were obtained and compared. The damage patterns of failed specimens of notched and unnotched were examined with the aid of high-definition camera and stereomicroscope. The results of stress-strain relationships showed that the slight nonlinearity of the curves were observed for these two specimens, which was associated with the plastic deformation of localized resin. The damage patterns of notched and unnotched specimens at different temperatures proved that damage and plastic deformation were two simultaneous mechanisms and it was prominent in the notched. It was the overstress accommodation mechanism that led to a relative high strength rentention for the notched and a reduction of the hole sensitivity. The results obtained in this paper indicated that GF/PPS can be used as secondary aircraft structures at elevated temperatures higher than its Tg.https://doi.org/10.1051/matecconf/201710801009 |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Wang Yue Zhang Jipeng Zhang Jiazhen Zhou Zhengong |
spellingShingle |
Wang Yue Zhang Jipeng Zhang Jiazhen Zhou Zhengong Temperature Effects on Mechanical Properties of Woven Thermoplastic Composites for Secondary Aircraft Structure Applications MATEC Web of Conferences |
author_facet |
Wang Yue Zhang Jipeng Zhang Jiazhen Zhou Zhengong |
author_sort |
Wang Yue |
title |
Temperature Effects on Mechanical Properties of Woven Thermoplastic Composites for Secondary Aircraft Structure Applications |
title_short |
Temperature Effects on Mechanical Properties of Woven Thermoplastic Composites for Secondary Aircraft Structure Applications |
title_full |
Temperature Effects on Mechanical Properties of Woven Thermoplastic Composites for Secondary Aircraft Structure Applications |
title_fullStr |
Temperature Effects on Mechanical Properties of Woven Thermoplastic Composites for Secondary Aircraft Structure Applications |
title_full_unstemmed |
Temperature Effects on Mechanical Properties of Woven Thermoplastic Composites for Secondary Aircraft Structure Applications |
title_sort |
temperature effects on mechanical properties of woven thermoplastic composites for secondary aircraft structure applications |
publisher |
EDP Sciences |
series |
MATEC Web of Conferences |
issn |
2261-236X |
publishDate |
2017-01-01 |
description |
The effect of temperature on the mechanical behavior of 8-H satin woven glass fabric/polyethylene sulfide (GF/PPS) was investigated in this paper. Static-tensile tests were both conducted on notched and unnotched specimens at typical temperatures (ambient, 95°C and 125°C) based on the glass transition temperatures (Tg) of the neat resin and composite, their strength and moduli were obtained and compared. The damage patterns of failed specimens of notched and unnotched were examined with the aid of high-definition camera and stereomicroscope. The results of stress-strain relationships showed that the slight nonlinearity of the curves were observed for these two specimens, which was associated with the plastic deformation of localized resin. The damage patterns of notched and unnotched specimens at different temperatures proved that damage and plastic deformation were two simultaneous mechanisms and it was prominent in the notched. It was the overstress accommodation mechanism that led to a relative high strength rentention for the notched and a reduction of the hole sensitivity. The results obtained in this paper indicated that GF/PPS can be used as secondary aircraft structures at elevated temperatures higher than its Tg. |
url |
https://doi.org/10.1051/matecconf/201710801009 |
work_keys_str_mv |
AT wangyue temperatureeffectsonmechanicalpropertiesofwoventhermoplasticcompositesforsecondaryaircraftstructureapplications AT zhangjipeng temperatureeffectsonmechanicalpropertiesofwoventhermoplasticcompositesforsecondaryaircraftstructureapplications AT zhangjiazhen temperatureeffectsonmechanicalpropertiesofwoventhermoplasticcompositesforsecondaryaircraftstructureapplications AT zhouzhengong temperatureeffectsonmechanicalpropertiesofwoventhermoplasticcompositesforsecondaryaircraftstructureapplications |
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1724312870695469056 |