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Multiaxial Fatigue Life Prediction Based on Nonlinear Continuum Damage Mechanics and Critical Plane Method

机译:基于非线性连续体损伤力学和临界平面方法的多轴疲劳寿命预测

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摘要

A new multiaxial fatigue life prediction model has been proposed in this paper. The concepts of nonlinear continuum damage mechanics and critical plane criteria were incorporated in the proposed model. The shear strain-based damage control parameter was chosen to account for multiaxial fatigue damage under constant amplitude loading. Fatigue tests were conducted on nickel-based superalloy GH4169 tubular specimens at the temperature of 400?°C under proportional and nonproportional loading. The proposed method was checked against the multiaxial fatigue test data of GH4169. Most of prediction results are within a factor of two scatter band of the test results.
机译:本文提出了一种新的多轴疲劳寿命预测模型。 非线性连续体损伤力学和临界平面标准的概念被纳入拟议的模型。 选择剪切应变损伤控制参数以考虑在恒定幅度负载下的多轴疲劳损伤。 在比例和非储能负荷下,在400Ω℃的温度下在镍基超合金GH4169管状标本上进行疲劳试验。 针对GH4169的多轴疲劳试验数据检查所提出的方法。 大多数预测结果都在测试结果的两个散射带内。

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