93 resultados para LI-7


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<正> Ⅰ.概况 国际等离子体化学会议(ISPC)每两年举行一次,主要交流等离子体化学如下几方面的研究和发展情况:合成,诊断,等离子体刻蚀,等离子体沉积和聚合,模型,表面作用以及熔化、气化、等离子体喷涂等。ISPC-7由荷兰Ejndhoven技术大学负责组织,Philips公司支持,在Philips会议中心举行。会议期1985年7月1—5日。第一天样品展览,

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The microstructures and the characteristics of water-atomized, nitrogen gas-atomized Al powders and ultrasonic argon gas-atomized Al-Li alloy powder were investigated by means of metallography, SEM, Auger electron spectroscopy and X-ray diffraction techniques. Rapidly solidified powders were explosively consolidated into different sized cylinders under various explosive parameters. The explosively consolidated compacts have been tested and analysed for density microhardness, retention of rapidly solidified microstructures, interparticle bonding, fractography and lattice distortion. It is shown that the explosive consolidation technique is an effective method for compacting rapidly solidified powders. The characteristics of surface layers play a very important role in determining the effectiveness of the joints sintered, and the Al-Li alloy explosive compacts present an abnormal softening appearance compared to the original powder.

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The effect of the particle cover over the density interface between two layers of fluids and of the suspended solid particles in the upper turbulcnt layer on the turbulent entrainment has been studied experimentally. The entrainment distance D is a function of the time of power: D=kt, where =0.200-0.130p. For suspended particles in the upper layer and pure 2-layer fluid is equal to 0.200, but the value of k for the suspended particles is smaller than that for the pure 2-layer fluid. The non-dimensional entrainment velocity is E=KRiln, where n=1.50+0.93 p. It is shown that the particle cover over the interface changes the power of Ril in the entrainment and hinders the turbulent entrainment. The variation rule of E for the suspended particles is the same as that for the pure 2-layer fluid, but the K value of the former is smaller than that of the latter. The turbulent mixing mechanism has been discussed.

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Fatigue crack growth and its threshold are investigated at a stress ratio of 0.5 for the three-point bend specimen made of Austenitic stainless steel. The effect of grain size on the crack tip plastic deformation is investigated. The results show that the threshold value Δkth increases linearly with the square root of grain size d and the growth rate is slower for materials with larger grain size. The plastic zone size and ratio for different grain sizes are different at the threshold. The maximum stress intensity factor is kmax and σys is the yield strength. At the same time, the characteristics of the plastic deformation development is discontinuous and anti-symmetric as the growth rate is increased from 2·10—8 to 10−7 mm/cycle.

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在山西省万家寨引黄入晋工程总干线 7#隧洞的开挖和衬砌的应力应变分析中 ,为确定土体c、Φ值和邓肯 -张模型参数 ,分别进行了加载试验和卸载试验 ,本文对用两种试验获得的模型参数进行有限元变形分析的结果进行比较。

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在地震等灾变的发生之前,会出现一定的前兆现象.文中通过实验方法对这些前兆现象之一的态矢量的异常变化进行了研究.实验使用声发射技术(Acoustic Emission),对三轴应力条件下岩石试件内部微裂纹的产生和扩展进行了记录.实验结果表明在岩石试件最终破坏之前,表征态矢量的相关参量都发生了异常明显的变化,这表明态矢量的异常变化可以被用作为岩石等脆性材料灾变的前兆,使用态矢量方法可以对脆性材料的破坏乃至地震作出预测.

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The microstructure of Nd_{60}Al_{10}Ni_{10}Cu_{20-x}Fex (x = 0, 5, 7, 10, 15, 20) alloys can change from homogeneous phase to a composite structure consisting of amorphous phase plus clusters or nanocrystals by adjusting the Fe content. The effect of microstructure on the plastic deformation behavior in this alloy system is studied by using nanoindentation. The alloys with homogeneous amorphous structure exhibit pronounced flow serrations during the loading process of nanoindentation. The addition of Fe changes the plastic deformation behavior remarkablely. No flow serration is observed in the alloys with high Fe content for the indentation depth of 500 nm. The mechanism for the change of plastic serrated flow behavior is discussed.

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This book elucidates the methods of molecular gas dynamics or rarefied gas dynamics which treat the problems of gas flows when the discrete molecular effects of the gas prevail under the circumstances of low density, the emphases being stressed on the basis of the methods, the direct simulation Monte Carlo method applied to the simulation of non-equilibrium effects and the frontier subjects related to low speed microscale rarefied gas flows. It provides a solid basis for the study of molecular gas dynamics for senior students and graduates in the aerospace and mechanical engineering departments of universities and colleges. It gives a general acquaintance of modern developments of rarefied gas dynamics in various regimes and leads to the frontier topics of non-equilibrium rarefied gas dynamics and low speed microscale gas dynamics. It will be also of benefit to the scientific and technical researchers engaged in aerospace high altitude aerodynamic force and heating design and in the research on gas flow in MEMS

  • 目次内容                                                                
[1]  Molecular structure and energy states (21)  
 
[2]  Some basic concepts of kinetic theory (51)  
 
[3]  Interaction of molecules with solid surface (131)  
 
[4]  Free molecular flow (159)  
 
[5]  Continuum models (191)  
 
[6]  Transitional regime (231)  
 
[7]  Direct simulation Monte-Carlo (DSMC) method (275)  
 
[8]  Microscale slow gas flows, information preservation method (317)  
 
[App. I]  Gas properties (367)  
 
[App. II]  Some integrals (369)  
 
[App. III]  Sampling from a prescribed distribution (375)  
 
[App. IV]  Program of the couette flow (383)  
 
Subject Index (399)  

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本书阐明了板壳断裂理论的基础。论证了Reissner型板壳断裂理论的科学性、经典板壳断裂理论的缺陷及在一定范围内仍具有的实用价值;介绍了作者所创意的研究Reissner型板壳断裂纹尖端场的方法等。

目录

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全书以命令行方式通过大量教学实例和工程应用实例,介绍了建立模型、求解和结果后处理的全过程。

目 录

前言

第1篇教学实例篇

第1章简单拉压杆结构

1.1铰接杆在外力作用下的变形

1.2人字形屋架的静力分析

1.3超静定拉压杆的反力计算

1.4平行杆件与刚性梁连接的热应力问题

1.5端部有间隙的杆的热膨胀

第2章梁的弯曲问题

2.1等截面简单超静定梁的平面弯曲分析

2.2工字形截面外伸梁的平面弯曲

2.3矩形截面梁的纵横弯曲分析

2.4悬臂梁的双向弯曲

2.5 圆形截面悬臂杆的弯扭组合变形

2.6悬臂等强度梁的弯曲

2.7弹性地基半无限长梁在端部力和力偶作用下的变形

2.8偏心受压杆的大变形分析

第3章杆系稳定性计算

3.1利用梁单元计算压杆稳定性

3.2利用实体单元计算压杆稳定性

3.3悬臂压杆的过曲屈分析

3.4平面钢架的平面外失稳

第4章实体模型应力分析

4.1 均布荷载作用下深梁的变形和应力

4.2一对集中力作用下的圆环

4.3用实体单元分析变截面杆的拉伸

4.4用二维实体单元分析等截面悬臂梁的平面弯曲

4.5变截面悬臂梁在端部集中力作用下的平面静力分析

4.6纯弯曲悬臂曲梁的二维静力分析

4.7端部集中力作用的悬臂圆环曲梁平面弯曲的三维分析

4.8均匀拉力作用下含圆孔板的孔边应力集中

4.9两端固定的厚壁管道在自重作用下的变形和应力

第5章膜和薄壳问题

5.1含椭圆孔的椭圆薄膜在外部张力作用下的静力分析

5.2圆形薄膜大变形静力分析

5.3柱形容器在内压作用下的静力分析

5.4圆柱形薄壳在均匀内压作用下的静力分析

第6章板的弯曲和壳体计算

6.1简支和固支圆板的在不同荷载作用下的弯曲

6.2悬臂长板的大挠度弯曲

6.3用壳体单元分析受均布荷载作用的固支圆板大挠度弯曲

6.4利用拉伸操作建立膨胀弯管模型

6.5两端简支开口柱壳在自重作用下的静力分析

6.6圆筒在一对横向集中力作用下的变形

6.7两边简支开口柱壳在集中力作用下的大变形曲屈

第7章简单振动系统

7.1单自由度弹簧质量系统的频率计算

7.2悬索自由振动的频率

7.3用弹簧单元连接的圆盘的扭转振动

7.4圆杆连接圆盘的扭转振动

7.5钻杆的扭转自由振动

第8章梁的振动分析

8.1简支梁的自振频率计算

8.2 自由―自由梁的纵向自由振动

8.3有轴向压力作用的简支梁的自由振动

8.4用壳体单元计算悬臂等强度梁的自由振动

8.5矩形截面薄壁悬臂梁的自由振动

第9章膜板和实体振动

9.1 圆形张紧薄膜的自由振动

9.2薄膜二维非轴对称自由振动分析

9.3薄膜三维非轴对称振动分析

9.4悬臂长板的自由振动频率

9.5悬臂宽板的模态分析

9.6固支圆板的自由振动

9.7用实体单元分析圆环的振动

9.8机翼模型的振动分析

第1 0章平面建模分析和三维实体建模

10.1 带三个圆孔的平面支座分析

10.2角支座应力分析

10.3 体斜支座的实体建模

10.4四分之一车轮的实体建模

10.5轴承支座的实体建模

第1 1章最优化设计

11.1概述

11.2最优化问题框架

11.3 ANSYS优化设计流程

11.4变截面悬臂梁的外形形状优化

11.5平面刚架的优化设计

第12章层合板和断裂力学

12.1 四边简支方形层合板在均布外载作用下的变形

12.2均布拉力作用下含裂纹板的应力强度因子计算

第2篇工程应用篇

第13章用APDL实现空间网壳结构参数化建模

13.1 K系列球面网壳结构的特点和建模

13.1.1 K系列球面网壳的特点

13.1.2几何描述

13.1.3杆件连接关系

13.2参数化设计语言APDL介绍

13.2.1参数和表达式

13.2.2 ANSYS 中的基本指令

13.2.3分支和循环

13.3用户界面设计语言UIDL介绍

13.3.1 单行参数输入

13.3.2多行参数输入

13.4网壳建模程序设计

13.4.1模型建立的步骤

13.4.2节点坐标计算

13.4.3单元连接

13.4.4变量说明

13.4.5节点坐标计算公式

13.4.6主框图说明

13.4.7单元连接关系定义

13.4.8源程序

13.5程序使用说明

13.5.1加载程序

13.5.2界面说明

13.5.3注意事项

13.6应用举例

13.6.1基本参数

13.6.2输入数据并生成模型

13.6.3输入单元参数和荷载后开始计算

13.6.4选择结果输出方式

第14章塔式起重机静动力分析

14.1塔式起重机基本概念

14.2塔式起重机拓扑模型

14.3塔机模型受力分析

14.3.1部件受力特征分析

14.3.2截面参数定义

14.3.3自重荷载和配重

14.3.4选用合适的分析模型。

14.3.5 固定塔身底部的4个节点

14.4塔机建模程序设计

14.4.1塔身节点计算和单元连接

14.4.2塔顶建模

14.4.3塔臂建模

14.4.4平衡臂和斜拉索建模

14.5塔机静力分析

14.6塔机模态分析

14.7塔机静动力分析程序

第15章长柱形天然气罐在内压作用下的静力分析

15.1概述

15.2建立模型

15.3利用轴对称壳单元SHELL51计算

15.3.1单元基本性质和约定

15.3.2求解过程

15.3.3源程序

15.3.4计算结果

15.3.5简体部分理论解

15.3.6结果讨论

15.4利用8节点2D实体单元PLANE82单元计算

15.4.1建立模型

15.4.2计算过程

15.4.3计算结果及讨论

15.4.4源程序

15.5用20节点3D实体单元solid95计算1/4模型

15.5.1建立1/4三维模型

15.5.2计算步骤

15.5.3计算结果分析

15.5.4与弹性力学解答的对比

15.5.5计算程序

附录

附录A常用结构单元参考

附录B结构分析命令速查

参考文献

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Effects of wall temperature on stabilities of hypersonic boundary layer over a 7-degree half-cone-angle blunt cone are studied by using both direct numerical simulation (DNS) and linear stability theory (LST) analysis. Four isothermal wall cases with Tw/T0= 0.5, 0.7, 0.8 and 0.9, as well as an adiabatic wall case are considered. Results of both DNS and LST indicate that wall temperature has significant effects on the growth of disturbance waves. Cooling the surface accelerates unstable Mack II mode waves and decelerates the first mode (Tollmien–Schlichting mode) waves. LST results show that growth rate of the most unstable Mack II mode waves for the cases of cold wall Tw/T0=0.5 and 0.7 are about 45% and 25% larger than that for the adiabatic wall, respectively. Numerical results show that surface cooling modifies the profiles of rdut/dyn and temperature in the boundary layers, and thus changes the stability haracteristic of the boundary layers, and then effects on the growth of unstable waves. The results of DNS indicate that the disturbances with the frequency range from about 119.4 to 179.1 kHz, including the most unstable Mack modes, produce strong mode competition in the downstream region from about 11 to 100 nose radii. And adiabatic wall enhances the amplitudes of disturbance according to the results of DNS, although the LST indicates that the growth rate of the disturbance of cold wall is larger. That because the growth of the disturbance does not only depend on the development of the second unstable mode.