闭孔泡沫铝的塑性泊松比

在表征闭孔泡沫铝的力学性能中,塑性泊松比是较为重要的参数之一。本文应用Kelvin十四面体模型构建出不同相对密度的闭孔泡沫铝三维细观模型并采用LS-DYNA对所得细观模型进行单轴准静态压缩计算。数值模拟分析发现,随着轴向应变的增加,泡沫铝泊松比-轴向应变曲线呈倒S形,存在峰值和极小值,曲线变化规律与泡沫铝胞孔的变形有密切关系。根据泊松比-轴向应变曲线与胞孔变形之间的关系,给出了平均塑性泊松比的定义。计算结果显示,随着相对密度的提高,闭孔泡沫铝的平均塑性泊松比增大。当闭孔泡沫铝的相对密度低于0.1时,其平均塑性泊松比接近于零,计算中可以忽略;当闭孔泡沫铝相对密 度大于0.1时,其平均塑性泊松比随相对密度的增加而呈线性从0.17增加到0.5     

PVDF压电薄膜用于Hopkinson压杆测量泡沫金属的动态性能

首先对PVDF(polyvinylidene fluoride)压电薄膜在不同温度不同压力作用下的响应进行了系统的试验研究。然后在Hopkinson压杆系统的透射杆之间夹上PVDF压电薄膜,对其动态响应进行了检验。最后应用这个镶嵌PVDF压电薄膜的Hopkinson压杆系统,测试了泡沫铜材料在不同应变率下的应力应变关系。结果表明:(1)PVDF压电薄膜的压电常数D33是随温度和压力而变,实际应用时应对其进行标定;(2)PVDF压电薄膜可有效的用于Hopkinson压杆系统来测试低强度泡沫材料或低阻抗材料的动态响应;(3)当应变率小于0.1/s时,泡沫铜的塑性流动应力对应变率不敏感,在约400/s到5000/s应变率范围,应变小于40%下泡沫铜对应变率也不敏感。但当应变大于约20%,应变率高于400/s时,与低应变率下的值比较,塑性流动应力的应变率敏感性增加。     

泡沫铝率相关性能的有限元模拟

构建了三维随机分布球形泡孔模型,模拟开、闭孔混合结构泡沫铝材料的微细观结构,并通过有限元方法计算了10~104 s-1应变率范围内、孔隙率35%~65%泡沫铝材料的率相关性以及应变率和相对密度变化对泡沫铝动态压缩力学性能的影响。研究表明:中、低应变率下,泡沫铝材料率相关性能主要取决于基体材料的应变率敏感性;高应变率下,泡沫铝材料率相关性能受基体材料的应变率敏感性以及微结构惯性联合作用,且相对密度较低泡沫铝材料的微结构惯性效应更显著。     

通孔泡沫铝的动态压缩行为

在SHPB装置上对渗流法制备的通孔泡沫铝进行了动态压缩实验,研究了相对密度为0.341~0.419的通孔泡沫铝在10-3~2000 s-1应变率范围内的压缩响应特征和应变率相关性,并用扫描电镜（scanning electron microscope,SEM)分析了泡沫铝的压缩变形特征。实验结果表明,通孔泡沫铝有明显应变率效应,随应变率上升,泡沫铝流动应力提高。SEM观察结果揭示,在动态压缩下,通孔泡沫铝宏观上均匀变形,微观变形机制以泡孔横向伸展坍塌为主。     

电磁加载下7075铝环的膨胀断裂模式转变研究

利用电磁膨胀环实验技术,研究了7075铝环在2700～8700 s?1拉伸加载应变率下的断裂模式转变现象。实验结果表明:在低应变率下,铝环的断裂受最大正应力控制,发生拉伸断裂;在高应变率下,铝环的断裂受最大剪应力控制,发生剪切断裂;在中应变率下,铝环的断裂同时受最大正应力和最大剪应力控制,为拉伸和剪切同时存在的拉剪混合断裂模式;随着应变率的增加,铝环的破片数量呈先增加、再减小、最后增加的趋势,破片数量变化拐点与断裂模式转变点基本吻合。     

钛合金在低温下的高速变形特性和绝热剪切

采用SHPB技术在室温和低温下,对相钛合金TB-2的高速变形特性和绝热剪切进行了宏观和微观研究。结果表明,TB-2是一个对应变率和温度敏感的材料,其热粘塑性本构特性可表为 =(0+E1（1+gln/0）（1-（T-Tn） /Tn）显微观察表明,TB2在低温下比在常温下对绝热剪切更敏感。低温下绝热剪切带的形态和结构也和常温下有所不同。把文献[9]所建议的绝热剪切的热粘塑性失稳准则,应用到不同的环境温度下,本文建议了一个既依赖于应变和应变率,又依赖于环境温度的三变量准则。理论预示和试验结果符合较好。     

闭孔泡沫铝泊松比及三轴压缩变形模式

在闭孔泡沫铝的唯象本构模型中, 泊松比是一个非常关键的参数, 为了探究闭孔泡沫铝泊松比变化规律研究结果存在分歧的原因, 认识闭孔泡沫铝泊松比变化规律中特征点的物理意义, 采用数值模拟方法, 建立了闭孔泡沫铝的3D-Voronoi模型及2D-Voronoi模型, 对模型进行侧面位移耦合单轴压缩边界条件下的仿真分析; 基于闭孔泡沫铝本构模型的唯象特性, 对闭孔泡沫铝变形模式的研究同样十分重要, 为明确其三轴压缩下的变形模式, 对闭孔泡沫铝的3D-Voronoi模型进行侧面位移受限轴向压缩边界条件下的仿真分析. 研究结果表明, 常规壳单元接触中的厚度减薄特性是闭孔泡沫铝泊松比变化规律的研究结论存在分歧的原因, 但厚度减薄不影响泡沫铝模型致密前胞孔结构的变形模式; 闭孔泡沫铝泊松比的准确变化规律为“增高?降低?再增高”的“S”型曲线, 并且, 曲线极大值对应闭孔泡沫铝吸能效率的增速下降点; 等比压缩应力状态下, 闭孔泡沫铝存在四种侧面变形模式, 分别为“(短期)压缩变形→膨胀变形”、“压缩变形→膨胀变形→压缩变形→膨胀变形”、“压缩变形→(短期)膨胀变形”及“压缩变形”.      

描述大应变率范围下材料响应的粘塑性本构模型

以位错动力学理论中的Ｏｒｗａｎ和Ｇｉｌｍａｎ关系为基础建立描述率相关材料非弹性响应的基本方程，选择材料准静态实验的单轴响应作为强化演化的规律，并考虑应变率敏感程度随变形产生变化的特性，建立了适用于大应变率范围内率相关材料的统一型粘塑性本构模型。对铝１１００－０在应变率范围１０－５～１０４ｓ－１内产生的有限塑性应变的单轴响应进行了理论预测，与Ｋｈａｎ和Ｈｕａｎｇ［１］的实验数据及模型预测结果进行了比较，结果表明本文模型具有较高的预测精度，在高应变率和较大应变下不容忽视率敏感参数随变形的变化。     

铝-锂合金动态扭转实验研究

利用霍普金森扭杆（Torsional Split-Hopkinson Bar）技术对三种不同成份或状态的铝-锂合金材料的动态应力-应变-应变率关系进行了实验测定。应变率范围由1300s-1到2600s-1,研究表明随着应变率的提高,三种不同成份或状态的铝-锂合金材料的韧性和强度都有不同程度的提高。对剪切带的初步观察发现,随应变率的增加,剪切带有变窄的趋势。     

高氮奥氏体不锈钢高温动态响应特性及本构关系

在293~873 K的环境下,采用分离式霍普金森杆装置对高氮钢试样进行了102~103 s-1应变率下的动态加载实验。结合准静态实验结果,分析了应变率和温度对材料塑性流动特性的影响。结果表明:高氮钢的动态力学行为具有很强的应变率敏感性和温度敏感性。当应变率达到400 s-1或更高时,流动应力随应变率的增加显著升高;在同一应变率下,流动应力随温度的降低明显升高。研究了温度和应变率耦合效应对材料塑性行为的影响,得出温度软化效应在高氮钢高温动态塑性变形中起主导作用。基于经典的Johnson-Cook（J-C）模型,通过对实验数据的分析,得出了高氮钢材料的修正J-C本构方程,经验证修正J-C方程预测结果与实验结果吻合。     

5083H111铝合金宽应变率拉伸动态本构模型

结合5083H111铝合金较宽应变率范围2×10-4 ~ 4×102s-1内的拉伸实验数据,揭示该铝合金的拉伸“V”型率效应特征,分析对数应变率敏感系数λ和切线模量Et的应变率和应变相关性,进而通过对Johnson-Cook模型的修正来建立合理描述5083H111铝合金较宽应变率范围内的动态拉伸本构模型。建立的动态本构模型中,流动应力包括应变率相关和应变相关两部分。该模型合理描述了5083H111铝合金的拉伸“V”型率效应特征,预测结果与实验结果较为一致。另外,结合破坏应变的对数应变率敏感系数β,得到了拉伸破坏应变预测方程,其预测结果也与实验结果基本一致。     

泡沫铝合金动态力学性能实验研究

利用分离式霍布金森压杆(SHPB)实验技术和MTS材料实验机对两组不同孔径、不同密度的开孔泡沫铝合金进行了准静态和动态压缩实验研究。实验结果表明:泡沫铝合金的静态和动态变形过程均具有泡沫材料变形的三个阶段特征。开孔泡沫铝合金的变形是均匀变化过程，并不出现局部的变形带。与相对密度对力学性能的影响相比，孔径大小的影响可以忽略不计。在考察的应变率范围内，屈服应力对应变率并不很敏感。     

The characteristics of plastic flow and a physically-based model for 3003 Al–Mn alloy upon a wide range of strain rates and temperatures

The uniaxial compressive responses of 3003 Al–Mn alloy upon strain rates ranging from 0.001/s to about 10⁴/s with initial temperatures from 77 K to 800 K were investigated. Instron servohydraulic testing machine and enhanced split Hopkinson bar facilities have been employed in such uniaxial compressive loading tests. The maximum true strain up to 80% has been achieved. The following observations have been obtained from the experimental results: 1) 3003 Al–Mn alloy presents remarkable ductility and plasticity at low temperatures and high strain rates; 2) its plastic flow stress strongly depends on the applied temperatures and strain rates; 3) the temperature history during deformation strongly affects the microstructure evolution within the material. Finally, paralleled with the systematic experimental investigations, a physically-based model was developed based on the mechanism of dislocation kinetics. The model predictions are compared with the experimental results, and a good agreement has been observed.     

Dynamic strain aging and related instabilities: experimental,theoretical and numerical aspects

Experimental data from uniaxial tensile tests on smooth and notched specimens of aluminium alloy 5083-H116 show that the material exhibits negative strain-rate sensitivity for strain rates within a certain range. The negative strain-rate dependence, which is attributed to dynamic strain aging, leads to serrated stress–strain curves, discontinuous plastic flow and propagating deformation bands during plastic straining (also denoted as the Portevin–Le Chatelier effect). Band analysis and linear perturbation analysis are performed using simple elastic-viscoplastic constitutive equations that include negative strain-rate sensitivity in a simplified manner. The negative strain-rate sensitivity allows for jumps in the plastic strain rate, which in turn permits the existence of localisation bands for the elastic-viscoplastic model. The simple elastic-viscoplastic constitutive model has been implemented in LS-DYNA, and non-linear finite element simulations of smooth and notched tensile test specimens are performed, allowing more detailed investigations into the effects of the negative strain-rate sensitivity on the material's behaviour.     

应力作用下NiTi形状记忆合金微结构演化的相场模拟及其本征应变率敏感性

基于Ginzburg-Landau动力学控制方程建立了NiTi形状记忆合金非等温相场模型,实现了对NiTi合金内应力诱导马氏体相变的数值模拟。同时将晶界能密度引入系统局部自由能密度,从而考虑多晶系统中晶界的重要作用。数值计算了单晶和多晶NiTi形状记忆合金在单轴机械载荷作用下微结构的动态演化过程和宏观力学行为,并重点研究了晶粒尺寸为60 nm的NiTi纳米多晶在低应变率下（0.0005～15 s?1）力学行为的本征应变率敏感性。研究结果表明,单晶NiTi合金系统高温拉伸-卸载过程中马氏体相变均匀发生,未形成奥氏体-马氏体界面。而纳米多晶系统在加载阶段出现了马氏体带的形成-扩展现象,在卸载阶段出现了马氏体带的收缩-消失现象。相同外载作用过程中,NiTi单晶系统的宏观应力-应变曲线具有更大的滞回环面积,拥有更优的超弹性变形能力。计算结果显示,在中低应变率下纳米晶NiTi形状记忆合金应力-应变关系表现出较明显的应变率相关性,应变率升高导致材料相变应力提升。这一应变率相关性主要源于相场模型中外加载荷速率与马氏体空间演化速度的相互竞争关系。     

A study of localisation in dual-phase high-strength steels under dynamic loading using digital image correlation and FE analysis

Tensile tests were conducted on dual-phase high-strength steel in a Split-Hopkinson Tension Bar at a strain-rate in the range of 150–600/s and in a servo-hydraulic testing machine at a strain-rate between 10^?3 and 10⁰/s. A novel specimen design was utilized for the Hopkinson bar tests of this sheet material. Digital image correlation was used together with high-speed photography to study strain localisation in the tensile specimens at high rates of strain. By using digital image correlation, it is possible to obtain in-plane displacement and strain fields during non-uniform deformation of the gauge section, and accordingly the strains associated with diffuse and localised necking may be determined. The full-field measurements in high strain-rate tests reveal that strain localisation started even before the maximum load was attained in the specimen. An elasto-viscoplastic constitutive model is used to predict the observed stress–strain behaviour and strain localisation for the dual-phase steel. Numerical simulations of dynamic tensile tests were performed using the non-linear explicit FE code LS-DYNA. Simulations were done with shell (plane stress) and brick elements. Good correlation between experiments and numerical predictions was achieved, in terms of engineering stress–strain behaviour, deformed geometry and strain fields. However, mesh density plays a role in the localisation of deformation in numerical simulations, particularly for the shell element analysis.     

Strain-rate history and temperature effects on the torsional-shear behavior of a mild steel

Previous investigations on the effects of strain-rate and temperature histories on the mechanical behavior of steel are briefly reviewed. A study is presented on the influence of strain rate and strain-rate history on the shear behavior of a mild steel, over a wide range of temperature Experiments were performed on thin-walled tubular specimens of short gage length, using a torsional split-Hopkinson-bar apparatus adapted to permit quasi-static as well as dynamic straining at different temperatures. The constant-rate behavior was first measured at nominal strain rates of 10^?3 and 10³ s^?1 for ?150, ?100, ?50, 20, 200 and 400°C. Tests were then carried out, at the same temperatures, in which the strain rate was suddenly increased during deformation from the lower to the higher rate at various large values of plastic strain. The increase in rate occurred in a time of the order of 20 μs so that relatively little change of strain took place during the jump. The low strain-rate results show a well-defined elastic limit but no yield drop, a small yield plateau is found at room temperature. The subsequent strain hardening shows a maximum at 200°C, when serrated flow occurs and the ductility is reduced. The high strain-rate results show a considerable drop of stress at yield. The post-yield flow stress decreases steadily with increasing temperature, throughout the temperature range investigated. At room temperature and below, the strain-hardening rate becomes negative at large strains. The adiabatic temperature rise in the dynamic tests was computed on the assumption that the plastic work is entirely converted to heat. This enabled the isothermal dynamic stress-strain curves to be calculated, and showed that considerable thermal softening took place. The initial response to a strain-rate jump is approximately elastic, and has a magnitude which increases with decrease of testing temperature; it is little affected by the amount of prestrain. At 200 and 400° C, a yield drop occurs after the initial stress increment. The post-jump flow stress is always greater than that for the same strain in a constant-rate dynamic test, the strain-hardening rate becoming negative at large strains or low testing temperature. This observed effect of strain-rate history cannot be explained by the thermal softening accompanying dynamic deformation. These and other results concerning total ductility under various strain-rate and temperature conditions show that strain-rate history strongly affects the mechanical behavior of the mild steel tested and, hence, should be taken into account in the formulation of constitutive equations for that material.     

The study on the compressive behavior of ptfe/al energetic composite

金属/氟聚合物含能复合材料是一类新型的高级含能材料. 研究了室温下Al含量和应变 率对PTFE/Al含能复合材料压缩性能和反应性能的影响,所加载的应变率为6\times 10^{-3}s^{-1}\sim8\times 10^{3}s^{ -1}. 材料压缩性能的应变 率效应明显：与静态加载相比,动态加载下材料模量和强度明显提 高,但应变降低. 材料的损伤过程主要包括塑性变形、开裂和反应3部分. 随着Al含量的增 加,材料准静态和动态压缩强度均呈先升后降的趋势,在 Al含量为35\%时达到 最高值102.6 MPa和154 MPa; 引发反应所需加载的应变率增加,但对应的应力值 差别不明显,基本在165 MPa左右, 材料引发后反应完全性降低.