Fatigue reliability and sensitivity analysis of turbine disk with fuzzy failure status

Low-cycle fatigue is typical failure mode of aero-engine turbine disk, traditional reliability analysis method based on the binary state assumption has certain limitations for turbine disk reliability evaluation, because it doesn't consider the change of damage strength parameter caused by load...

وصف كامل

التفاصيل البيبلوغرافية
الحاوية / القاعدة:Xibei Gongye Daxue Xuebao
المؤلفون الرئيسيون: Huang Xiaoyu, Wang Pan, Li Haihe, Zhang Zheng
التنسيق: مقال
اللغة:الصينية
منشور في: EDP Sciences 2021-12-01
الموضوعات:
الوصول للمادة أونلاين:https://www.jnwpu.org/articles/jnwpu/full_html/2021/06/jnwpu2021396p1312/jnwpu2021396p1312.html