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The thermal-vibration coupling nonlinear fatigue life prediction of the space shuttle antenna

机译:航天飞机天线的热振动耦合非线性疲劳寿命预测

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Considering the severe vibrations and harsh temperature changes in space crafts' launching and landing processes, this paper presents a novel thermal-vibration coupling nonlinear fatigue life prediction model. Focusing on the effect of temperature in the fatigue residual strength degradation, the modified Corten-Dolan model is proposed to describe the cumulative damage under the thermal-vibration coupling. The simulation indicates that the proposed model is more accurate as compared to traditional methods.
机译:考虑到空间工艺发射和着陆过程中严重的振动和苛刻的温度变化,本文提出了一种新型热振动耦合非线性疲劳寿命预测模型。提出了对疲劳残余强度降解的温度效果,提出了改进的Corten-Dolan模型来描述热振动耦合下的累积损伤。模拟表明,与传统方法相比,所提出的模型更准确。

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