Anisotropic FCGR behaviour in hot-rolled Mg-3Al-0.5Ce alloy

IF 15.8 1区 材料科学 Q1 METALLURGY & METALLURGICAL ENGINEERING
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Abstract

In this work, anisotropic fatigue crack growth rate (FCGR) behaviour in a hot-rolled Mg-3wt%Al-0.5wt%Ce alloy was investigated using compact tension (CT) specimens with notch (an) parallel to the rolling direction (RD) and transverse direction (TD). The FCGR tests were conducted at a constant load ratio (R = 0.1) and maximum stress intensity factor (KMax = 15.6 MPa√m) to investigate the crack closure effect. For both constant R and KMax conditions: (i) the load-displacement curves for every loading cycle were linear for an ∥ to RD and TD, indicating no crack closure; (ii) the FCGR was found to be lower for an ∥ RD than an ∥ TD over the entire stress intensity factor range (ΔK). The hot-rolled sample contained long-aligned Al11Ce3 intermetallic phase within grain boundaries that are elongated along RD. During the FCGR test, {101¯2}101¯1 extension twins (ET) with lamellae ∼⊥ and c-axis to these elongated intermetallics along RD developed irrespective of the notch orientation. During the loading cycle, these intermetallics along RD generate back-stresses, reducing the in-plane tensile stress and to crack-tip to 0 for an ∥ to RD and TD, respectively. Hence, lenticular ET and , with c-axis and to crack path activates, leading to trans and inter lamellar crack for an ∥ to RD and TD, respectively, and anisotropic FCGR. Translamellar crack in an ∥ RD reduces the FCGR due to plastic energy dissipation as perceived by comparatively more geometrically necessary boundaries (GNBs). On the other hand, faster FCGR was obtained for an ∥ TD due to interlamellar cracking. Thus, the crack growth through the matrix-ET interfaces was favoured due to strain incompatibility. The Fractography for an ∥ RD shows smaller elongated grooves along crack propagation, which indicates crack arrest. However, larger elongated grooves for an ∥ TD indicated easy crack propagation due to favourable interlamellar crack.

热轧 Mg-3Al-0.5Ce 合金中的各向异性 FCGR 行为
本研究使用缺口(an)平行于轧制方向(RD)和横向方向(TD)的紧凑拉伸(CT)试样,研究了热轧 Mg-3wt%Al-0.5wt%Ce 合金的各向异性疲劳裂纹生长率(FCGR)行为。FCGR 试验在恒定载荷比 (R = 0.1) 和最大应力强度因子 (KMax = 15.6 MPa√m) 下进行,以研究裂纹闭合效应。在恒定 R 和 KMax 条件下:(i) RD 和 TD ∥ 时,每个加载周期的载荷-位移曲线呈线性,表明没有裂纹闭合;(ii) 在整个应力强度因子范围内(ΔK),RD ∥ 时的 FCGR 低于 TD ∥ 时的 FCGR。热轧样品的晶界中含有长排列的 Al11Ce3 金属间相,这些金属间相沿 RD 延伸。在 FCGR 试验中,无论缺口方向如何,都会出现{101¯2}〈101¯1〉延伸孪晶 (ET),其薄片∼⊥和 c 轴∼∥均与这些沿 RD 延伸的金属间相一致。在加载周期中,这些沿 RD 的金属间隙会产生背应力,使 RD 和 TD ∥ 时的面内拉应力 ∼∥ 和裂纹尖端拉应力 ∼⊥ 分别减小到 ∼0。因此,透镜状 ET ∼⊥和 ∼∥,c 轴 ∼∥和 ∼⊥至裂纹路径激活,导致 RD 和 TD ∥分别出现跨层和层间裂纹,以及各向异性 FCGR。RD ∥中的跨层裂纹由于相对较多的几何必要边界(GNB)所产生的塑性能量耗散而降低了 FCGR。另一方面,由于层间裂纹,∥TD 的 FCGR 更快。因此,由于应变的不相容性,裂纹有利于通过基体-ET界面生长。RD ∥的分形图显示出沿裂纹扩展方向较小的细长沟槽,这表明裂纹停止了扩展。然而,∥TD 的拉长沟槽较大,表明由于有利于层间裂纹,裂纹易于扩展。
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来源期刊
Journal of Magnesium and Alloys
Journal of Magnesium and Alloys Engineering-Mechanics of Materials
CiteScore
20.20
自引率
14.80%
发文量
52
审稿时长
59 days
期刊介绍: The Journal of Magnesium and Alloys serves as a global platform for both theoretical and experimental studies in magnesium science and engineering. It welcomes submissions investigating various scientific and engineering factors impacting the metallurgy, processing, microstructure, properties, and applications of magnesium and alloys. The journal covers all aspects of magnesium and alloy research, including raw materials, alloy casting, extrusion and deformation, corrosion and surface treatment, joining and machining, simulation and modeling, microstructure evolution and mechanical properties, new alloy development, magnesium-based composites, bio-materials and energy materials, applications, and recycling.
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