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Effect of mean shear stress on the fatigue strength of notched components under multiaxial stress state

机译：平均剪切应力对多轴应力状态下缺口组分疲劳强度的影响

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M. Bennebach; T. Palin-Luc; A. Messager;
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年度 2018
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1. Predicting the multiaxial fatigue limit and the multiaxial high-cycle fatigue life based on the unified equivalent shear stress from axial strength characteristics with various waveforms [J] . Go Matsubara, Atsushi Hayashida, Daichi Kano International Journal of Fatigue . 2018,第JULa期

机译：根据具有各种波形的轴向强度特性，基于统一的等效剪应力，预测多轴疲劳极限和多轴高周疲劳寿命
2. Comparison of different one-parameter damage laws and local stress-strain approaches in multiaxial fatigue life assessment of notched components [J] . R. Branco, J.D. Costa, L.P. Borrego, International Journal of Fatigue . 2021,第Octa期

机译：不同单参数损伤法律和局部应力 - 应变方法对缺口组分的多轴疲劳寿命评估
3. Gradient elasticity: a transformative stress analysis tool to design notched components against uniaxial/multiaxial high-cycle fatigue [J] . C BAGNI, H ASKES, L SUSMEL Fatigue & fracture of engineering materials and structures . 2016,第8期

机译：梯度弹性：一种变换应力分析工具，用于设计缺口构件以抵抗单轴/多轴高周疲劳
4. Effect of mean shear stress on the fatigue strength of notched components under multiaxial stress state. [C] . M. Bennebach, T. Palin-Luc, A. Messager International Conference on Fatigue Design . 2018

机译：平均剪切应力对多轴应力状态下缺口组分疲劳强度的影响。
5. Fatigue Behavior under Multiaxial Stress States Including Notch Effects and Variable Amplitude Loading [D] . Gates, Nicholas R. 2016

机译：多轴应力状态下的疲劳行为包括缺口效应和可变幅度载荷
6. Validating the Methods to Process the Stress Path in Multiaxial High-Cycle Fatigue Criteria [O] . Jan Papuga, Eva Cízová, Aleksander Karolczuk 2021

机译：在多轴高周期疲劳标准中验证处理应力路径的方法
7. Effect of Static and Intermittent Shear Stress on the Fatigue Strength of Notched Components under Combined Rotating Bending and Torsion [O] . Bennebach M., Palin-Luc T. 2015

机译：静态和间歇剪切应力对组合弯曲弯曲与扭转下缺口构件疲劳强度的影响
8. FATIGUE STRENGTHS OF AIRCRAFT MATERIALS AXIAL-LOAD FATIGUE TESTS ON NOTCHED SHEET SPECIMENS OF 24S-T3 AND 75S-T6 ALUMINUM ALLOYS AND OF SAE 4130 STEEL WITH STRESS-CONCENTRATION FACTOR OF 1.5 [R] . H. J. Grover, W. S. Hyler, L. R. Jackson 1952

机译：飞机材料的疲劳强度轴承疲劳试验在24s-T3和75s-T6铝合金以及saE 4130钢的缺口板试样上具有1.5的应力集中系数

Effect of mean shear stress on the fatigue strength of notched components under multiaxial stress state

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