Risk evaluation in failure mode and effects analysis of aircraft turbine rotor blades using Dempster–Shafer evidence theory under uncertainty
Risk evaluation in failure mode and effects analysis of aircraft turbine rotor blades using Dempster–Shafer evidence theory under uncertainty
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DOI：
10.1016/j.engfailanal.2011.06.014
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发表时间：
2011-12
影响因子：
4
通讯作者：
Jianping Yang;Hongzhong Huang;Liping He;Shun‐Peng Zhu;Dunwei Wen
中科院分区：
文献类型：
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作者：
Jianping Yang;Hongzhong Huang;Liping He;Shun‐Peng Zhu;Dunwei Wen
