航空用TC21钛合金变截面模锻件的显微组织和力学性能不均匀性分析
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Inhomogeneity Analyses of Microstructure and Mechanical Properties of TC21 Titanium Alloy Variable Cross-section Die Forgings for Aviation
YANG Jie, HUANG Sensen, YIN Hui, ZHAI Ruizhi, MA Yingjie, XIANG Wei, LUO Hengjun, LEI Jiafeng, YANG Rui
图10 图1a中Ⅱ处沿不同方向的典型冲击曲线
Fig.10 Typical displacement-load curves at position Ⅱ in Fig.1a along LD (a) and ND (b) (Fmax—maximum load, WE—impact energy obtained from the experimental curve, WF—impact energy obtained by fitting the curve, Wi—crack initiation energy, Wp—crack propagation energy)