排序方式: 共有26条查询结果,搜索用时 15 毫秒
1.
2.
Comparison of formation and evolution of radiation-induced defects in pure Ni and Ni-Co-Fe medium-entropy alloy
下载免费PDF全文
![点击此处可从《中国物理 B》网站下载免费的PDF全文](/ch/ext_images/free.gif)
High-entropy alloys (HEAs) and medium-entropy alloys (MEAs) have attracted a great deal of attention for developing nuclear materials because of their excellent irradiation tolerance. Herein, formation and evolution of radiation-induced defects in NiCoFe MEA and pure Ni are investigated and compared using molecular dynamics simulation. It is observed that the defect recombination rate of ternary NiCoFe MEA is higher than that of pure Ni, which is mainly because, in the process of cascade collision, the energy dissipated through atom displacement decreases with increasing the chemical disorder. Consequently, the heat peak phase lasts longer, and the recombination time of the radiation defects (interstitial atoms and vacancies) is likewise longer, with fewer deleterious defects. Moreover, by studying the formation and evolution of dislocation loops in Ni-Co-Fe alloys and Ni, it is found that the stacking fault energy in Ni-Co-Fe decreases as the elemental composition increases, facilitating the formation of ideal stacking fault tetrahedron structures. Hence, these findings shed new light on studying the formation and evolution of radiation-induced defects in MEAs. 相似文献
3.
4.
5.
通过二维Yee氏元胞割分法中的时域有限差分(FDTD)法对光子晶体光纤中二维导行电磁波在TE波,TM波中x,y,z方向矢量数值变换以此来建立入射激励光源在光子晶体中传播行为的基本理论模型,为此通过对Courant稳定条件及BS-PML吸收边界等参数进行设定与计算机程序数值仿真相结合的方式分析了入射光波在不同时间段不同色散值所产生的电场波与磁场波之间特性关系.研究结果表明:即色散数值偏大时,其光子晶体光纤中TM波能量转移更为显著. 相似文献
6.
7.
8.
9.
轴流压气机转子近叶尖流动的试验和数值研究之二:近失速工况流动特征分析 总被引:4,自引:0,他引:4
采用机匣壁动态压力测量技术对某高速亚音轴流压气机转子中转数可压条件下不同工况点叶尖流场进行了测量.在对近失速工况点试验测量结果进行详细分析的基础上,结合全通道非定常的数值模拟对试验观察到的流动现象进行了解释。结果表明:随着工况点向失速边界点推进,叶尖区出现的非定常流动现象(旋转不稳定性)增强,且该非定常流动现象的活动频率随流场的调整在一定带宽范围内变化;通过非定常数值模拟结果与试验测量结果的对比分析表明,叶尖通道中以一定周期活动的TSV的出现是旋转不稳定性流动现象出现的流体动力学机制。 相似文献
10.
以某叶尖失速型的轴流压气机转子为研究对象,开展了无叶尖喷气以及喷气量为1%边界流量情况的全通道非定常数值模拟。数值探针监测结果表明:不喷气时出现了与实验测量结果一致的突尖型失速,而喷气情况下出现的是模态型失速。对比叶尖喷气下不同工况点的瞬态流场发现:在喷气流影响的径向范围内,喷嘴右侧通道中间隙泄漏流和吸力面尾缘分离耦合作用形成的流动阻塞,随着流量的减小逆转子转动方向沿周向扩展;而喷气流影响的径向范围外,喷嘴左侧通道中吸力面尾缘分离形成的流动阻塞顺转子转动方向沿周向扩展。这种流动阻塞格局的发展演化是喷气情况下出现模态扰动的原因。 相似文献