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机译:7075-T651铝制凸耳中钢衬套过盈配合的变化会导致疲劳寿命变化
University of Alabama in Huntsville, Department of Mechanical and Aerospace Engineering, United States,US Army, Aviation Engineering Directorate, United States;
University of Alabama in Huntsville, Department of Mechanical and Aerospace Engineering, United States;
aerospace; aluminum alloy; fatigue strength; life prediction; S-N curves;
机译:通过冷膨胀,干涉配件及其组合提高2297-T87铝 - 锂合金凸耳的疲劳寿命
机译:过盈配合的铝合金7075-T651螺栓紧固样品的疲劳行为
机译:干涉的疲劳行为适合Al-Alloy 7075-T651试样进行螺栓拧紧
机译:用于提高疲劳寿命和结构完整性的高抗干扰配合套管安装
机译:7075-T651铝制凸耳中钢衬套过盈配合的变化会导致疲劳寿命变化。
机译:钢铝轴承衬套锻造的挑战
机译:利用表面声波研究7075-T651铝和4340钢的细小疲劳裂纹
机译:冷作工艺和干涉配合衬套对带孔聚碳酸酯试样疲劳寿命的影响