112 resultados para MC-RR


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本文设计并制备了具有优良的强韧性能和高温性能的激光熔覆涂层。利用 SEM、TEMEY X-射线衍射仪等研究了涂层的化学成分、宏微观结构及其转变机制,同时研究了涂层强韧性及耐高温磨损性能及其影响机制。对激光溶覆涂层进行了合金化、微观组织、强韧化机制、加工工艺性能设计。合金系为 Fe-Cr-C-W-Ni,成分配比(质量分数),Fe:52-60%, Cr:24-30%, C:5-6%, W:4.5-7.5%, Ni:5-6%。强化机制为两相强化、亚结构强化及固溶强化,其中强化相为合金碳化物,基体相为合金元素过饱和度极高的韧性奥氏体。亚共晶及过共晶组织的领先凝固相分别为奥氏体及 M_7C_3 合金碳化物,两相共晶组织均为韧性相奥氏体和强化相 M_7C_3 合金碳化物。加工工艺控制领先凝固相的结构、组织演化及力学性能。熔覆组织在高温时效过程中形成大量新的碳化物。在过饱和奥氏体内部,可弥散析出细小的 Mc、M_2C 及 M_(23)C_6碳化物;在奥氏体与 M_7C_3 相界面,亚稳相M_7C_3发生原位转变,形成 M_(23)C_6 及 M_6C碳化物。激光熔覆合金具有较高的综合力学性能,熔覆涂层有高的显微硬度、优良的抗回火稳定性、显著的二次硬化特征、优异的抗磨粒磨损和冲击磨损性能。Fe-Cr-C-W-Ni 激光熔覆合金具有较低的裂纹形成倾向和良好的表面成形性能,这与奥氏体较高的高温韧塑性及合金的低熔点共晶特征密切相关;实验及理论分析表明,通过调整合金成分、激光工艺参数和后续热处理工艺,可获得具有不同强韧性能的熔覆涂层。

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《高等断裂力学》系统论述断裂力学的基本概念、理论基础、力学原理、分析方法以及断裂力学的实验测定和工程应用。深入阐明了断裂力学各个重要发展阶段的新颖学术思想和原创性工作,同时融会贯通地介绍了国内学者在作者熟悉的若干领域内的创造性贡献。  《高等断裂力学》共14章。第1章介绍断裂力学的历史背景和发展脉络;第2~5章介绍线弹性断裂力学;第6~8章论述弹塑性断裂力学;第9及第10章分别介绍疲劳裂纹扩展和界面裂纹;第11~14章阐述裂纹体弹性动力学和裂纹动态扩展。  《高等断裂力学》适合从事断裂力学研究和应用的科技工作者及工程师使用和参考,也可供力学专业的高年级本科生和研究生阅读参考.

目录

丛书序
序言
第1章 引论
1.1 历史背景
1.2 工程意义
1.3 脆性破坏特征
1.4 断裂力学起源与发展
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第2章 线弹性断裂力学
2.1 裂纹尖端弹性应力场
2.2 应力强度因子理论
2.3 裂纹扩展能量原理
2.4 裂纹尖端塑性区
2.5 厚度对KC的影响
2.6 裂纹扩展阻力曲线
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第3章 应力强度因子分析方法
3.1 Williams级数展开与边界配置法
3.2 复变函数方法
3.3 权函数法
3.4 积分变换法
3.5 奇异积分方程
3.6 有限单元法
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第4章 平面应变断裂韧性
4.1 标准试样
4.2 试样取向与制备
4.3 测试仪器和有效性分析
4.4 KR曲线测试
参考文献

第5章 复合型裂纹的脆断理论
5.1 复合型裂纹变形特征
5.2 应力参数准则
5.3 分支裂纹应力强度因子
5.4 能量释放率准则
5.5 复合型裂纹脆断试验
5.6 理论与实验比较
5.7 塑性变形对金属材料复合型裂纹脆性断裂的影响
参考文献

第6章 弹塑性断裂力学
6.1 J积分原理
6.2 HRR奇性场
6.3 J积分准则
6.4 J控制扩展
6.5 断裂韧性JIC测试
6.6 Dugdale模型
6.7 带状颈缩区模型
6.8 裂纹张开位移准则
参考文献

第7章 裂纹顶端弹塑性高阶场
7.1 高阶场基本方程
7.2 一阶场和二阶场
7.3 高阶场前5项完整结果
7.4 J-Q双参数方法
7.5 J-k断裂准则
7.6 平面应力裂端弹塑性场
参考文献

第8章 理想弹塑性介质扩展裂纹尖端场
8.1 v=0.5时的裂尖渐近场
8.2 v<0.5时的裂尖场
8.3 理想弹塑性介质Ⅲ型扩展裂纹
8.4 扩展裂纹与J积分
参考文献

第9章 疲劳裂纹扩展
9.1 等幅载荷下裂纹扩展
9.2 影响疲劳裂纹扩展的因素
9.3 裂纹闭合效应
94疲劳裂纹扩展门槛值确定
95等幅载荷下疲劳裂纹寿命预测
96变幅载荷下疲劳寿命预测
97缺口根部的疲劳裂纹
参考文献

第10章 界面裂纹
101弹性界面力学
102界面裂纹弹性断裂力学
10.3 典型的界面断裂问题
10.4 界面断裂试验
参考文献

第11章 弹性动力学基本概念及方法
11.1 动态惯性效应
11.2 线弹性动力学基本方程
11.3 复变解析函数
11.4 Laplace变换
11.5 Wiener-Hopf分解
11.6 动态断裂的能量概念
参考文献

第12章 静止裂纹的弹性动力学基本解
121突加反平面剪切载荷
12.2 突加裂纹面正压力
12.3 突加平面内剪切应力情况
124有限长裂纹面突加载荷情况
12.5 动态载荷裂纹的起始扩展
参考文献

第13章 均匀材料中动态扩展裂纹
13.1 动态裂纹定常扩展
13,2裂纹面上集中剪切力
133黏结区模型
13.4 Broberg问题
13.5 对称扩展剪切裂纹
136时间无关载荷作用下裂纹扩展
13.7 时间相关载荷作用下裂纹扩展
13.8 II型超剪切波扩展裂纹
13.9 裂纹尖端超弹性区对I、II型裂纹速度的影响
参考文献

第14章 双材料界面动态裂纹扩展
14.1 准静态动态裂纹扩展
14.2 双材料界面裂纹含接触区跨音速扩展
14.3 界面裂纹的超音速扩展
参考文献
索引

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The critical wedge angle (CWA) for the transition from regular reflection (RR) to Mach reflection (MR) of a cellular detonation wave is studied numerically by an improved space-time conservation element and solution element method together with a two-step chemical reaction model. The accuracy of that numerical way is verified by simulating cellular detonation reflections at a 19.3∘ wedge. The planar and cellular detonation reflections over 45∘–55∘ wedges are also simulated. When the cellular detonation wave is over a 50∘ wedge, numerical results show a new phenomenon that RR and MR occur alternately. The transition process between RR and MR is investigated with the local pressure contours. Numerical analysis shows that the cellular structure is the essential reason for the new phenomenon and the CWA of detonation reflection is not a certain angle but an angle range.

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In order to obtain the distribution rules of in situ stress and mining-induced stress of Beiminghe Iron Mine, the stress relief method by overcoring was used to measure the in situ stress, and the MC type bore-hole stress gauge was adopted to measure the mining-induced stress. In the in situ stress measuring, the technique of improved hollow inclusion cells was adopted, which can realize complete temperature compensation. Based on the measuring results, the distribution model of in situ stress was established and analyzed. The in situ stress measuring result shows that the maximum horizontal stress is 1.75-2.45 times of vertical stress and almost 1.83 times of the minimum horizontal stress in this mineral field. And the mining-induced stress measuring result shows that, according to the magnitude of front abutment pressure the stress region can be separated into stress-relaxed area, stress-concentrated area and initial stress area. At the -50 m mining level of this mine, the range of stress-relaxed area is 0-3 m before mining face; the range of stress-concentrated area is 3-55 m before mining face, and the maximum mining-induced stress is 16.5-17.5 MPa, which is 15-20 m from the mining face. The coefficient of stress concentration is 1.85.

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More and more piezoelectric materials and structures have been used for structure control in aviation and aerospace industry. More efficient and convenient computation method for large complex structure with piezoelectric actuation devices is required. A load simulation method of piezoelectric actuation is presented in this paper. By this method, the freedom degree of finite element simulation is significantly reduced, the difficulty in defining in-plane voltage for multi-layers piezoelectric composite is overcome and the transfer computation between material main direction and the element main direction is simplified. The concept of simulation load is comprehensible and suitable for engineers of structure strength in shape and vibration control, thereby is valuable for promoting the application of piezoelectric material and structures in practical aviation and aerospace fields.

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采用透射电镜及附带能谱(TEM-EDS)对K418高温合金涡轮盘和42CrMo合金钢转轴激光焊焊缝的微观组织进行了分析.结果表明:焊缝主要由树枝状非平衡凝固的FeCrNiC(γ)固溶体组成,此外,还有少量细小、弥散的Ni_3Alγ'相、Laves颗粒和少量MC碳化物分布在树枝晶之间区域;根据热动力学原理对形成这一组织特征的原因进行了简要讨论.

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Photoelectron angular distributions produced in above-threshold ionization (ATI) are analysed using a nonperturbative scattering theory. The numerical results are in good qualitative agreement with recent measurements. Our study shows that the origin of the jet-like structure arises from the inherent properties of the ATI process and not from the angular momentum of either the initial or the excited states of the atom.