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...
| الحاوية / القاعدة: | Xibei Gongye Daxue Xuebao |
|---|---|
| المؤلفون الرئيسيون: | , , , |
| التنسيق: | مقال |
| اللغة: | الصينية |
| منشور في: |
EDP Sciences
2021-12-01
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| الموضوعات: | |
| الوصول للمادة أونلاين: | https://www.jnwpu.org/articles/jnwpu/full_html/2021/06/jnwpu2021396p1312/jnwpu2021396p1312.html |
