厚向异性板应力应变强度表述方法讨论

从希尔 (Hill)正交各向异性体二次屈服函数出发 ,可以导出厚向异性板应力强度 (等效应力 )与应变强度 (等效应变 )的两组表达式 ;本文讨论了采用两组不同表述方法的选择 ,并利用单向拉伸与双向等拉两种实验作了可比性的分析比较     

Effect of temperature on mechanical behavior of AZ31 magnesium alloy

Strain rate sensitivity and tension/compression asymmetry of AZ31 magnesium alloy at different temperatures and strainrates were investigated.Both of mechanical behaviors are temperature dependent.Strain rate sensitivity increases with increasingtemperature.Thermally activated slip is the source of strain rate sensitivity.At the temperature below or near 373 K,strain ratesensitivity is very little.Tension/compression asymmetry in yielding decreases with increasing temperature.Twinning is the reasonof tension/compression asymmetry.At the temperature above or near 573 K,the material shows little tension/compressionasymmetry of the flow stress.     

DD3单晶镍基合金蠕变—疲劳及寿命预测

从应变范围区分法(SRP),应变能区分法(SEP)的有关概念出发,研究DD3单晶镍基合金拉—拉应力状态下的蠕变—疲劳性能和保持时间的影响,并对其进行了定量计算;同时,用应变能区分法的数值法(SEP—NCM)实现对拉—拉应力状态下蠕变—疲劳的寿命预测。     

STRAIN INDUCED STRUCTURAL TRANSITION OF INTERFACES AND TWINS IN A HOT－DEFORMED DUAL－PHASE TIAL ALLOY

ＳＴＲＡＩＮＩＮＤＵＣＥＤＳＴＲＵＣＴＵＲＡＬＴＲＡＮＳＩＴＩＯＮＯＦＩＮＴＥＲＦＡＣＥＳＡＮＤＴＷＩＮＳＩＮＡＨＯＴ－ＤＥＦＯＲＭＥＤＤＵＡＬ－ＰＨＡＳＥＴＩＡＬＡＬＬＯＹＣＨＥＮＧｕｏＦｉａｎｇ；ＷＡＮＧＪｉｎｇｕｏ；ＺＨＡＮＧＬｉｃｈｕｎａｎｄ...     

多通管塑挤胀形工艺的力学分析

讨论了以聚氨酯橡胶棒为胀形介质，采用塑挤胀形复合工艺把无缝管坯一次成形为多通管成品的加工方法，分析了多通管塑挤胀形过程，提出了“应变样条”分析法，进而分析了典型剖面上应力应变状态，讨论了成形力间应具备的合理的数值关系，以使变形区处于最有利于变形的超高的静水压力和合适的偏应力状态，获得尽可能长的支管。     

Effects of temperature and blank holding force on biaxial forming behavior of aluminum sheet alloys

Biaxial forming behavior is investigated for three aluminum sheet alloys (Al 5182 containing 1% Mn (5182+Mn), Al 5754, and 6111-T4) using a heated die and punch in the warm forming temperature range of 200–350 °C. It is found that, while all three alloys exhibit significant improvement in their formability compared with that at room temperature, the non-heat-treatable alloys 5182 + Mn and 5754 give higher part depths than that of heat-treatable 6111-T4. The formability generally increases with decreasing BHP (BHP), but increasing the forming temperature and/or BHP minimizes the wrinkling tendency and improves the forming performance. The stretchability of the sheet alloys increase with increasing temperature and increasing BHP. For the alloys and forming conditions involved in the current study, the formability, measured in terms of part depth, comes mainly from the drawing of metal into the die cavity, although stretching effects do influence the overall forming behavior. The optimum formability is achieved by setting the die temperature 50 °C higher than the punch temperature to enhance the drawing component. Setting the die temperature higher than the punch temperature also improves the strain distribution in a part in such a manner that postpones necking and fracture by altering the location of greatest thinning.     

含Ti微合金钢动态再结晶行为及模型研究

采用Gleeble 3800热力模拟实验机,研究了一种Ti微合金钢在850～1 150℃、0.1和1.0 s-1条件下的变形奥氏体的动态再结晶行为及再结晶后奥氏体晶粒尺寸的演化规律。结果表明:形变激活能与变形条件相关,随着应变速率的增加而增加;Avrami指数m同样与变形条件有关;对实验数据进行回归分析后建立的Ti微合金钢动态再结晶的特征应变、特征应力、动力学以及稳定状态晶粒尺寸的数学模型精度较高。     

分形及分维在单轴向三维编织复合材料拉伸实验中的应用

基于分形几何的计盒维数研究了三维编织复合材料拉伸实验的断裂样照,结果表明,该材料的断裂曲线具有统计自相似性,在不同的尺度范围内具有不同的空间分布格局;而计盒维数定量地表征了其尺度变化规律;准静态和低应变率加载条件下材料的分维数较大,表明其空间占据程度较大,曲线弯曲结构复杂,这是因为低应变率加载时材料内部结构断裂时间不同造成;而高应变率加载时,断裂曲线分维数较小,曲线空间占据小,弯曲结构比较简单,这是由高应变率加载时材料内部结构断裂时间差异缩小造成。     

Numerical Analysis of the Constrained Blister Test

The constrained blister test is investigated through finite element analysis to determine the applicabilities and the limitations of the new technique. Numerical results confirm that the strain energy release rate asymptotically approaches a constant value. These results also show that the test technique and the approximate solution for strain energy release rate are applicable for some practical cases.     

Failure load prediction of structural adhesive joints : Part 2: Experimental study

The objective of this study was to determine how the fracture of adhesive joints depends on elastic beam parameters describing the adherends and the applied loads. The basic specimen geometry was the cracked lap shear joint constructed of aluminium alloy with various adherend and bondline thicknesses. Loads were applied in different combinations of bending, tension and shear to generate a failure envelope for each adhesive and specimen geometry. It was found that crack propagation for precracked specimens occured at a critical strain energy release rate but was also a function of the G_I/G_II ratio and the bondline thickness. The experiments also showed that the loads required to propagate a crack in a precracked specimen were always lower than the loads required to break the fillet. Hence, by treating uncracked joints as being cracked, where the fictitious crack tip is assumed to coincide with the location of the fillet, a conservative estimate of the failure load is obtained.