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机译:截断载荷谱下2324-T39和7050-T7451铝合金的疲劳裂纹扩展行为和寿命预测
Institute of Solid Mechanics, School of Aeronautic Science and Engineering, Beihang University (BUM), Beijing 100191, China;
Department of Aerospace Engineering, School of Engineering, Cranfield University, Bedford MK43 0AL, UK;
fatigue crack growth; fatigue load spectra; crack branching; retardation; life prediction;
机译:截断频谱载荷下7050-T7451铝板在T-L和L-S取向破坏下的疲劳寿命和裂纹扩展速率评估
机译:低负荷截断水平对A1 2324-T39和A1 7050-T7451裂纹扩展的影响
机译:Spectrum Loading下2324-T39铝合金疲劳裂纹生长行为:实验和仿真
机译:喷丸7050-T7451铝合金的分析疲劳寿命预测
机译:不同载荷模式下沉淀强化CuNi2Si合金的疲劳裂纹扩展行为
机译:2324-T39和7050-T7451的疲劳裂纹扩展行为和寿命预测截断载荷谱下的铝合金
机译:设计应力水平和载荷频率下飞行模拟载荷下铝合金板材疲劳裂纹扩展