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机译:在拖动交替负载下评估预腐蚀的飞机机翼的疲劳寿命
Inst Tecnol Morelia Tecnol Nacl Mexico Ingn Mecan Dept Met Mecan Ave Tecnol 1500 Morelia 58120 Michoacan Mexico;
Inst Tecnol Morelia Tecnol Nacl Mexico Ingn Mecan Dept Met Mecan Ave Tecnol 1500 Morelia 58120 Michoacan Mexico;
Inst Tecnol Morelia Tecnol Nacl Mexico Ingn Mecan Dept Met Mecan Ave Tecnol 1500 Morelia 58120 Michoacan Mexico;
Inst Tecnol Morelia Tecnol Nacl Mexico Ingn Mat Dept Met Mecan Ave Tecnol 1500 Morelia 58120 Michoacan Mexico;
Inst Tecnol Morelia Tecnol Nacl Mexico Ingn Mecan Dept Met Mecan Ave Tecnol 1500 Morelia 58120 Michoacan Mexico;
Onera M6 wing; Pitting corrosion; Fatigue performance; Aluminum alloy 2024-T3; CFD;
机译:在拖动交替负载下评估预腐蚀的飞机机翼的疲劳寿命
机译:通过断裂载荷测试预测预腐蚀的2024-T3铝的疲劳寿命
机译:交替机翼压力载荷下飞机的运动
机译:多目标飞行控制,用于高纵横比柔性翼飞机的风阻最小化和负荷减轻
机译:通过断裂载荷试验预测预腐蚀2024-T3铝疲劳寿命的方法
机译:通过加速疲劳寿命测试对滑翔翼复合材料翼梁进行可靠性和使用寿命评估
机译:飞机翼面板紧固件孔的初始疲劳质量评估
机译:飞机加载程序修改对疲劳寿命和损伤累积的影响(Ⅰ) - 中心孔板试样负载峰的影响