摘要
对广泛应用于飞行器构件上的TC4(Ti-6Al-4V)钛合金,当受到激光冲击强化后的内部动态应力波传播特性建立模型,并进行数值模拟和实验验证。结果表明,实验测试与仿真结果比较接近,证明该文数值模拟的合理性,为后续实验研究提供了理论依据。
The transient transmission of stress wave of TC4 by LSP was analyzed in both FEM software ANSYS/LS-DYNA simulation and experimental studies.The experimental results is close to the simulation results which means the numerical simulation could play a directional role in the future studies of shock processing.
出处
《塑性工程学报》
CAS
CSCD
北大核心
2011年第4期79-84,共6页
Journal of Plasticity Engineering