机译:TC6合金高温变形本构方程的求解
College of Materials Science and Engineering Northwestern Polytechnical University 710072 Xi’an People’s Republic China;
College of Materials Science and Engineering Northwestern Polytechnical University 710072 Xi’an People’s Republic China;
College of Materials Science and Engineering Northwestern Polytechnical University 710072 Xi’an People’s Republic China;
Xi’an Aero-engine Company Group Ltd. 710021 Xi’an People’s Republic of China;
Xi’an Aero-engine Company Group Ltd. 710021 Xi’an People’s Republic of China;
Xi’an Aero-engine Company Group Ltd. 710021 Xi’an People’s Republic of China;
constitutive equation; flow stress; hot compression; titanium alloy;
机译:在高温变形下获得TC6合金的新本构方程
机译:考虑TC6钛合金晶粒尺寸的变形行为和新的本构方程
机译:Nitinol 60形状记忆合金本构方程与人工神经网络模型预测高温变形行为的比较研究
机译:低Cr-Mo合金蠕变变形及破裂机制述评下应力下蠕变损伤组成方程的发展
机译:基于统计-弹塑性-断裂模型的混凝土变形行为与本构方程
机译:冷径锻造6063铝合金半固体等温压缩的变形特性和本构剖面
机译:阿列尼斯和约翰逊烹饪组成型模型对Ti2AlnB基合金高温变形的比较研究
机译:描述结构合金高温非弹性行为的本构方程