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...
Main Authors: | , , , |
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Format: | Article |
Language: | zho |
Published: |
EDP Sciences
2021-12-01
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Series: | Xibei Gongye Daxue Xuebao |
Subjects: | |
Online Access: | https://www.jnwpu.org/articles/jnwpu/full_html/2021/06/jnwpu2021396p1312/jnwpu2021396p1312.html |