材料科学
断裂韧性
因科镍合金625
因科镍合金
巴黎法
强度因子
复合材料
紧凑拉伸试样
张力(地质)
断裂力学
应力集中
裂缝闭合
裂纹扩展阻力曲线
冶金
微观结构
极限抗拉强度
合金
作者
P. Ganesh,R. Kaul,C. P. Paul,Pragya Tiwari,Sanjay Rai,Rajendra Prasad,L. M. Kukreja
标识
DOI:10.1016/j.msea.2010.08.034
摘要
Fatigue crack growth and fracture toughness characteristics of laser rapid manufactured (LRMed) Inconel 625 compact tension specimens of thickness 12 and 25 mm were investigated. Fatigue crack propagation in all the specimens investigated in the stress intensity range (ΔK) of 14–38 MPa√m, exhibited stage II crack growth in Paris’ regime with nearly same slopes of crack growth per cycle versus ΔK plot. Fatigue crack growth rates in the LRMed specimens of present study were found to be lower than the reported values for wrought Inconel 625 in the ΔK range of 14–24 MPa√m and above this range they tended to coincide. X-ray diffraction patterns of the fractured surfaces revealed that the crack propagated along the growth direction of the specimens which was predominantly along the (1 1 1) plane. The fracture toughness values (J0.2) for LRMed Inconel 625 specimens were found to be in the range of about 200–255 kJ/m2. The LRMed specimens exhibited stable crack growth during the J-integral test.
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