机译:基于可靠性的复合材料飞机结构疲劳损伤预测框架
Department of Structural Engineering, University of California, San Diego, 9500 Gilman Lajolla, CA 92093-0085, United States;
Department of Structural Engineering, University of California, San Diego, 9500 Gilman Lajolla, CA 92093-0085, United States;
Department of Structural Engineering, University of California, San Diego, 9500 Gilman Lajolla, CA 92093-0085, United States;
The Engineering Institute, MS T-001, Los Alamos National Laboratory, Los Alamos, NM 87545, United States;
fatigue damage prognosis; structural health monitoring; probabilistic damage detection; damage evolution; system reliability; composite unmanned aerial vehicles;
机译:基于统一的飞机涡轮机磁盘设计优化框架
机译:稳固且基于可靠性的复合飞机机翼气动弹性剪裁框架
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机译:在不确定贝叶斯框架下结合多尺度退化故障模式的FRP复合材料疲劳损伤预后
机译:基于可靠性的航空航天复合结构粘结结构元件疲劳损伤预测框架
机译:带压痕损伤的后屈曲复合加劲结构的疲劳寿命和损伤容限
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机译:复合飞机结构在冲击,疲劳和环境条件下的认证。第二部分。复合材料疲劳的尺度效应。