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Evaluation of ultimate strength of high temperature composite materials for sst structures at elevated temperatures and after thermal aging

机译:高温和热老化后用于sst结构的高温复合材料的极限强度评估

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The objective of this experimental study was to evaluate the effect of thermal aging on the ultimate strength of three kinds of carbon/high-temperature polymer composite materials, which are current candidate structural materials for a super sonic transport of the next generation. The notched and unnotched panels, before being machined to specimens, next generation. The notched and unnotched panels, before being machined to specimens, next generation. The notched and unnotched panels, before being machined to specimens, were aged at 120 deg C and 180 deg C for up to 15,000 hours. Static tests at room and elevated temperatures before and after thermal aging provided the notched tensile, notched compressive, and short beam shear strengths. Moreover, the effects of five oxidation resistant treatments on notched compressive strength at 180 deg C were investigated after thermal aging of 5,000 hours at 180 deg C. The obtained results were presented and a possibility to develop an accelerated environment test methodology is examined.
机译:该实验研究的目的是评估热老化对三种碳/高温聚合物复合材料的极限强度的影响,这三种碳/高温聚合物复合材料是下一代超音速运输的当前候选结构材料。带槽口和无槽口的面板,在加工成标本之前,是下一代的。带槽口和无槽口的面板,在加工成标本之前,是下一代的。带缺口和无缺口的面板在加工成样品之前,先在120摄氏度和180摄氏度下老化15,000小时。热老化前后在室温和高温下的静态测试提供了缺口拉伸强度,缺口压缩强度和短梁剪切强度。此外,在180℃5,000小时的热老化后,研究了五种抗氧化处理对180℃下缺口抗压强度的影响。给出了所得结果,并检验了开发加速环境测试方法的可能性。

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