试验数据表明，激光冲击能有效地提高航空铝合金抗疲劳断裂的性能。
The test data show that laser shocking can improve effectively the properties of aviation aluminium alloys against fatigue fracture.
采用合理的平均力试验验证了模型的有效性，为进一步研究航空铝合金数控加工变形提供了可靠的边界条件。
The milling force model is validated according to cutting experiments and it can offer a reliable boundary condition for the further study of NC machining distortion of aviation aluminum-alloy.
从理论和实验两方面研究7050航空铝合金“单因素”本构模型中参数与温度的相关性。
To investigate the correlation between parameters of "single factor" constitutive model and temperature for 7050 aviation aluminum-alloy, theoretic analyses and material experiments were employed.
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