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Moisture Absorption Effects on Open-Hole Fully-Reversed Tension-Compression Fatigue Damage Tolerance of High Temperature Polymer Matrix Composites

机译:高温聚合物基质复合材料的高温聚合物基质复合材料的开放孔完全反向张力压缩疲劳损伤损伤的吸湿效应

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High performance aeronautics and aerospace applications of polymer matrix composites require long-term durability that is able to withstand exposure to extreme temperature, high relative humidity and oxidation environments. Moisture is one of critical environmental factors that can be damaging to composite properties. Generally, the absorption of moisture can reduce a glass transition temperature Tg and mechanical properties by matrix polymer plasticization, swelling, cracking and fiber/matrix interface damage. This paper is focused on moisture absorption effects and open-hole fatigue damage tolerance of the interesting and candidate high temperature polymer matrix composite materials for Next Generation Supersonic Civil Transportation.
机译:聚合物基质复合材料的高性能航空和航空航天应用需要长期耐久性,能够承受暴露于极端温度,高相对湿度和氧化环境。水分是可能对复合性质造成损害的关键环境因素之一。通常,通过基质聚合​​物塑化,溶胀,开裂和纤维/基质界面损坏,吸收水分的吸收可以降低玻璃化转变温度Tg和机械性能。本文的重点是对下一代超音速民用运输的有趣和候选高温聚合物基质复合材料的吸湿效应和开放式疲劳损伤耐受性。

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