摘要
介绍从NiTi形状记忆合金伪弹应力、回复应力与相变特征参量的内在联系出发,在实验的基础上利用计算机仿真技术建立回复应力与伪弹应力及温度、预应变之间关系的方法。
Based on the internal relations of pseudoelastic stress, recovery stress and martensitic transformation characteristic parameters of NiTi shape memory alloy, this paper describes the method for establishing the relationships between recovery stress and pseudoelastic stress, temperature and prestrain by the use of computer simulation technology.
出处
《航空制造工程》
1998年第2期46-48,共3页
Aviation Engineering & Maintenance
基金
国家自然科学青年基金
关键词
回复应力
计算机仿真
形状记忆合金
镍钛
NiTi shape memory alloy Martensitic transformation Recovery stressComputer simulation