无限冰介质中爆炸裂纹扩展机理与数值模拟

根据冰体力学性能,提出了无限淡水冰介质在爆炸冲击载荷下的压碎区及裂隙区的理论计算方法.利用大型有限元软件ANSYS/LS-DYNA模拟了爆炸载荷下无限区域冰体内裂纹扩展过程,模拟结果与实验结果基本一致,表明采用的损伤断裂模型能够较准确的反映无限冰介质动态力学性能及裂纹成形过程.数值模型可近似计算冰体中裂隙区的半径.数值计算值与理论计算值误差不超过5%,数值模拟结果与实验结果吻合,从而确定了无限区域冰体在-15℃时的基本破坏特征及范围.     

岩石结构面直剪力学特征的颗粒流宏细观分析

目前,由于颗粒尺寸和位置随机分布而产生的粗糙度,导致在模拟过程中出现应力集中现象,从而无法利用PFC2D准确模拟岩石结构面的剪切力学行为。为了避免以上弊端,采用结构面两侧颗粒组接触判别法分别对倾角为20°和30°的三角形单锯齿结构面进行不同法向应力下的直剪模拟。模拟结果与物理试验结果基本吻合,表明此模拟方法可以真实模拟岩石结构面剪切力学行为。为了进一步验证此模拟方法在天然结构面模拟试验中的可行性,利用PFC2D对Barton标准十条节理轮廓线模型进行不同法向应力下的直剪试验,模拟结果与理论值吻合,表明模拟方法具有可行性,为剪切破坏过程和机理分析提供可靠的理论依据,为研究粗糙结构面强度特征提供了一种思路。     

冻雨环境下润湿性表面覆冰黏附力测试方法

覆冰黏附力是仿生超疏水材料防结冰工程应用的关键技术指标之一. 根据覆冰样片降温过程中产生应变受冰层黏附力作用的原理, 提出利用电阻应变片传感器于模拟冻雨结冰环境下在线检测覆冰黏附力的方案. 应变片应变信号经数据采集、信号转换和软件处理, 实现了应变传感电压实时监测与在线显示, 结合受力分析对比计算出不同润湿性表面覆冰黏附力. 该方法可实时表征低温结冰环境下不同润湿性表面的结/融冰行为及覆冰黏附力变化趋势.     

方槽型纵骨船舶抗冰结构冰撞动响应实验研究

针对船舶冰区航行受冰体撞击结构损伤问题,以一种涉冰带船肩处船体板架结构为原型,提出了一种方槽型纵骨船舶抗冰结构型式。利用落锤冲击实验测试系统,对抗冰和原型加筋板架在相同冰体撞击工况下的结构动响应进行了实验研究,采用MSC.Dytran程序对板架受冰体撞击过程开展数值模拟,并与实验结果进行对比。结果表明,相同冰体撞击工况下,抗冰板架结构产生的撞击力比原型板架略大,冰体造成的抗冰板架结构最大凹陷深度小于原型板架。从船体外板结构损伤程度及对船体内部构件、设备防护作用的角度考虑,抗冰结构较原型具有一定的抗冰效果。研究成果可为冰区航行船或破冰船的抗冰结构设计提供参考。     

碳纤维复合材料冲击模型率相关修正方法与试验研究

目前先进航空发动机的风扇叶片均采用复合材料结构,为了研究其在工作过程中可能受到的冲击损伤,即碳纤维增强树脂基复合材料受到高速冲击后的损伤与破坏过程,对其准静态下的正交各向异性本构模型和失效准则进行修正,建立了应变率相关的三维动态本构及损伤模型．该模型考虑了材料模量、强度和断裂韧性与应变率的相关性,并采用基于断裂韧性的渐进损伤模式对刚度进行折减来控制破坏过程．开展了不同应变率下的动态试验,得到基体方向拉伸与剪切的动态响应数据,拟合得到相应的动态修正因子．将该模型结合修正因子植入数值软件进行仿真计算,分析结果表明,所建立的率相关本构及损伤模型能够更准确地模拟层合板受冲击过程的损伤和破坏,与试验吻合较好．     

含冰率影响下冻结道砟集料的三点弯曲试验研究

寒区有砟轨道中碎石道床在低温冰冻条件下的力学性能与常温明显不同，道砟颗粒间的冻结强度是影响道床动力学特性的一个重要参数。为进一步探究级配碎石在冻结条件下的弯曲力学性能，设计并制备了不同含冰率的冻结碎石集料试样，通过开展室内低温三点弯曲试验，研究了含冰率对冻结试样加载力-挠度曲线及弯曲强度的影响，并分析了冻结试样的断裂行为及断裂耗能情况。试验结果表明，试样的弯曲断裂失效过程可以分为脆性断裂和峰后应变软化型断裂两部分，加载力-挠度全曲线在脆性断裂时出现明显加载力跌落现象，而在应变软化型断裂过程中曲线下降趋势平缓。含冰率的提高显著增大了试样的弯曲强度，含冰率与弯曲强度之间的关系可近似线性表示。高含冰率试样弯曲脆性断裂时试样中部下方可观察到明显的受拉裂纹，并沿着道砟接触面向上不断扩展。含冰率较低时，试样脆性断裂耗能略高于应变软化型断裂耗能，其耗能占总消耗能量的70%以上，试样以脆性断裂为主；随着含冰率增大，试样脆性断裂能占比急速下降，应变软化型断裂逐渐占主体且不容忽视。     

单轴压缩下透明类岩石损伤演化特征研究

为研究岩石变形破坏模式及内部裂纹扩展过程,采用环氧树脂、固化剂、熔融石英砂与玻璃砂制备非均质、各向异性的新型透明类岩石,通过室内单轴压缩试验及颗粒流(PFC2D)数值模拟,分析了其破坏模式及裂纹演化过程。室内试验中,透明类岩石峰值强度在砂岩强度范围内的破坏模式与砂岩相似,呈现劈裂剪切混合破坏,裂纹发育大多以层理面为起始点;对比PFC2D数值模拟与室内试验,两者应力-应变曲线相似,最终破坏模式及过程基本一致;将透明类岩石的PFC2D裂纹累积演化曲线划分为无损伤、初始损伤、损伤发展、损伤加速发展、损伤破坏阶段,并确定了其损伤门槛值。本文试验结果,可为直接观察岩石内部裂纹扩展提供参考。     

胶结砂砾石层面直剪试验及破坏行为细观研究

本文采用宏观试验和细观模拟相结合的方法研究胶结砂砾石层面在剪切过程中的破坏行为．首先进行了不同法向应力作用下的胶结砂砾石层面直剪试验,获得了不同的剪切面破坏特征：随着法向应力的不断增加,剪切破坏面凹凸起伏程度、骨料脱落现象越发明显．其次为了深入探究层面破坏现象,按照室内试验采用的骨料级配粒径建立细观颗粒数值模型,结合物理试验对模型进行参数标定,并进行数值模型的层面直剪模拟和细观分析．结果表明,数值模型可以再现宏观直剪试验层面破坏特征;法向应力越大,层面区域颗粒发生错动和翻转的数量越多;层面破坏方式为颗粒间的张拉和剪切混合破坏,裂隙均集中在层面位置,随着法向应力的增加,裂隙的集中区域逐渐由“面”向“带”转变．     

Ti-6Al-4V弹体破坏模式对冲击反应的影响研究

Ti-6Al-4V材料是武器结构轻量化时的重要替代材料,其冲击反应将可能增加战斗部毁伤威力,但目前缺乏对其冲击反应条件及反应机理的研究。本文将采用试验与理论分析方法,研究结构破坏模式对Ti-6Al-4V材料冲击反应的影响,获得其冲击反应条件及反应机理。设计并开展了钛合金弹（头部与壳体均为钛合金）与复合弹（头部碳/碳复合材料、壳体空心钛合金圆柱）正侵彻混凝土试验,撞击速度在222~1008 m/s之间。钛合金弹激发了剧烈的氧化冲击反应,但复合弹未产生冲击反应。破坏模式宏细观分析显示,钛合金弹侵彻后宏观结构基本完整,仅表面发生摩擦磨损,以细观组织剪切变形为主要失效模式,形成尺寸在微米量级至百微米量级的颗粒碎片,碎片个数可高达3×106。复合弹的钛合金空心圆柱被撕裂成块,撕裂面沿剪切带方向发展,碎块尺寸在毫米或以上量级,个数至多百余个。碎片供氧和供热的效率均与碎片尺寸成反比,而特定供氧与供热条件下,碎片尺寸足够小是Ti-6Al-4V材料发生冲击反应的必要条件,这是钛合金弹发生冲击反应而钛合金空心圆柱无法激发冲击反应的本质原因。在具备冲击反应必要条件的前提下,碎片个数越多,冲击反应烈度越高。     

水动力作用下流冰撞击闸墩的动力响应研究

高寒地区河冰撞击河道的闸墩结构会产生极端冰载荷和冰激振动,水的动力效应使得碰撞过程更加复杂。采用任意拉格朗日-欧拉流固耦合方法,考虑作用在流冰和闸墩表面的流体力,建立了水-冰-闸墩耦合模型,探究了偶然极端条件下冰-闸墩碰撞的力学特性,设计了冰-砼碰撞实验。结果表明：冰-砼碰撞实验中,撞击力的模拟结果与实验结果吻合良好;对流固耦合的水动力效应分析发现,水-冰-闸墩耦合模型能够体现水的流体特性,在流冰撞击闸墩近场逼近过程中,初始时刻水的动力效应能够增加流冰的动能,撞击楔入闸墩过程中,水介质形成一个瞬态高压力场,产生水垫效应吸收冰体部分动能,从而抑制流冰运动;在不同流冰体积和压缩强度工况下,闸墩结构所承受的冰力随着流冰体积的增大而增大,流冰压缩强度对冰力的影响较小,流冰损伤与闸墩结构响应主要集中在碰撞接触区,流冰撞击闸墩结构引起冰激振动,流冰体积对闸墩振动加速度的影响较大,相同体积的流冰随着压缩强度的增大,振动幅值差异不明显,表明流冰体积是影响冰-闸墩碰撞的关键参数。     

Intersonic crack propagation in homogeneous media under shear-dominated loading: theoretical analysis

The mechanics of cohesive failure under mixed-mode loading is investigated for the case of a steadily propagating subsonic and intersonic dynamic crack subjected to a follower tensile and shear distributed load. The cohesive failure model chosen in this study is rate independent but accounts for the coupling between normal and tangential damage. Special emphasis is placed here on mixed-mode cases with predominantly shear loading. The analysis shows that the size of the mixed-mode cohesive zone is smaller than that obtained in the pure shear case. The relative extent of the shear and tensile cohesive damage zones depends on the crack speed and the mode mixity. In the intersonic regime, the failure process takes place exclusively in shear, even under remote mixed-mode loading conditions.     

Separation work analysis of cohesive law and consistently coupled cohesive law

An appropriate coupled cohesive law for predicting the mixed mode failure is established by combining normal separation and tangential separation of surfaces in the cohesive zone model (CZM) and the cohesive element method. The Xu-Needleman exponential cohesive law with the fully shear failure mechanism is one of the most popular models. Based on the proposed consistently coupled rule/principle, the Xu-Needleman law with the fully shear failure mechanism is proved to be a non-consistently coupled cohesive law by analyzing the surface separation work. It is shown that the Xu-Needleman law is only valid in the mixed mode fracture when the normal separation work equals the tangential separation work. Based on the consistently coupled principle and the modification of the Xu-Needleman law, a consistently coupled cohesive (CCC) law is given. It is shown that the proposed CCC law has already overcome the non-consistency defect of the Xu-Needleman law with great promise in mixed mode analyses.     

Separation work analysis of cohesive law and consistently coupled cohesive law

An appropriate coupled cohesive law for predicting the mixed mode failure is established by combining normal separation and tangential separation of surfaces in the cohesive zone model(CZM) and the cohesive element method.The Xu-Needleman exponential cohesive law with the fully shear failure mechanism is one of the most popular models.Based on the proposed consistently coupled rule/principle,the Xu-Needleman law with the fully shear failure mechanism is proved to be a non-consistently coupled cohesive la...     

不同加载状态下TA2钛合金绝热剪切破坏响应特性

一般认为绝热剪切现象在宏观上表现为材料动态本构失稳,即热软化大于应变硬化.本文采用帽型受迫剪切试样研究TA2钛合金的动态力学特性和本构失稳过程.首先对剪切区加载应力状态进行理论和数值分析,通过合理设计帽型试样,剪切区变形可近似按剪切状态处理;结合二维数字图像相关法(two-dimensional digital image correlation,DIC-2D)直接测试试样剪切区应变演化,给出帽型受迫剪切实验的等效应力-应变响应曲线.进一步,利用Hopkinson压杆对TA2钛合金开展动态压缩及帽型剪切对比试验研究,比较压缩、剪切试验得到的等效应力-应变曲线,采用"冻结"试样方法分析试样中绝热剪切局域化演化过程,探讨不同加载状态下TA2钛合金的绝热剪切破坏现象及其动态力学响应特性.实验结果表明,在塑性变形初始阶段,动态压缩及剪切加载下的等效应力-应变曲线符合较好,但随塑性损伤发展及绝热剪切带形成,两者出现分离,表明损伤及绝热剪切演化过程与应力状态相关.剪切试样实验得到的本构"软化"特性能够反映绝热剪切带起始、破坏演化过程的力学响应特性,而在动态压缩实验中,即使试样中已出现双锥形的绝热剪切带及局部裂纹分布,其表观等效应力-应变曲线并不出现软化特征,动态压缩实验无法得到关于绝热剪切起始、发展以及破坏的本构软化响应特性.     

Integrated numerical–experimental analysis of interfacial fatigue fracture in SnAgCu solder joints

In ball grid array (BGA) packages, solder balls are exposed to cyclic thermo-mechanical strains arising from the thermal mismatch between package components. Thermo-mechanical fatigue crack propagation in solder balls is almost always observed at the chip side of the bump/pad junction. The objective of the experimental part of this study is to characterize the bump/pad interface under fatigue loading. Fatigue specimens are prepared by reflowing Sn3.8Ag0.5Cu lead-free solder alloy on Ni/Au substrates. Obtained results show that fatigue damage evolution strongly depends on the microstructure. Applied strain and solder volume both have an influence on the fatigue damage mechanism. In the numerical part of the study, fatigue experiments are modeled using the finite element technique. A cohesive zone approach is used to predict the fatigue damage evolution in soldered connections. Crack propagation is simulated by an irreversible linear traction–separation cohesive zone law accompanied by a non-linear damage parameter. Cohesive zone elements are placed where failure is experimentally observed. Damage evolution parameters for normal and tangential interaction are scrutinized through dedicated fatigue tests in pure tensile and shear directions. The proposed cohesive zone model is quantitatively capable of describing fatigue failure in soldered joints, which can be further extended to a numerical life-time prediction tool in microelectronic packages.     

混凝土黏聚开裂模型若干进展

黏聚模型是用来描述混凝土断裂行为的基本模型, 首先介绍了混凝土的黏聚开裂模型的基本概念,总结了确定黏聚区的本构方程的各种方法,即直接单轴拉伸测试、J积分方法、R曲线法、柔度法和逆推法.然后介绍了黏聚模型在I型和复合型裂纹问题、疲劳断裂问题中的应用以及黏聚模型与混凝土尺寸效应的关系.最后对黏聚开裂模型与桥联模型、带状裂缝模型进行了比较和总结, 指出了该模型存在的问题, 并对其以后的发展方向提出了建议.      

Predicting the failure of ultrasonic spot welds by pull-out from sheet metal

A methodology for determining the cohesive fracture parameters associated with pull-out of spot welds is presented. Since failure of a spot weld by pull-out occurs by mixed-mode fracture of the base metal, the cohesive parameters for ductile fracture of an aluminum alloy were determined and then used to predict the failure of two very different spot-welded geometries. The fracture parameters (characteristic strength and toughness) associated with the shear and normal modes of ductile fracture in thin aluminum alloy coupons were determined by comparing experimental observations to numerical simulations in which a cohesive-fracture zone was embedded within a continuum representation of the sheet metal. These parameters were then used to predict the load–displacement curves for ultrasonically spot-welded joints in T-peel and lap-shear configurations. The predictions were in excellent agreement with the experimental data. The results of the present work indicate that cohesive-zone models may be very useful for design purposes, since both the strength and the energy absorbed by plastic deformation during weld pull-out can be predicted quite accurately.     

结构间隙对夹芯式复合装甲结构抗侵彻性能的影响

采用由厚度为8 mm的前置钛合金板、面密度为60 kg/m2的高强聚乙烯纤维增强复合材料层合板抗弹芯层、厚度为8 mm的后置钢板构成的夹芯式复合装甲,模拟舰船舷侧复合夹芯舱壁结构。根据面板与芯层间是否设置20 mm的间隙,将复合装甲结构定义为无间隙式、后间隙式及前后间隙式。为研究以上3种结构在55 g圆柱体弹高速冲击下的抗弹性能及破坏机理,开展了系列弹道实验,分析了钛合金板、高强聚乙烯纤维增强复合材料层合板芯层及钢质面板的破坏模式,探讨了结构间隙对复合装甲结构抗弹性能的影响。结果表明:前置钛合金板的破坏模式为剪切冲塞,靶板背弹面产生脆性断裂并伴随碎块崩落现象;聚乙烯纤维增强复合材料板的破坏模式及钢质背板的变形范围受间隙的影响较大,前置钛合金板受间隙影响较小;相同载荷侵彻下,间隙的存在有利于提高复合装甲结构的抗弹性能。     

SHEAR BEAM MODEL FOR INTERFACE FAILURE UNDER ANTIPLANE SHEAR (Ⅰ)—FUNDAMENTAL BEHAVIOR

The propagation of interlayer cracks and the resulting failure of the interface is a typical mode occurring in rock engineering and masonry structure. On the basis of the theory of elasto~plasticity and fracture mechanics, the shear beam model for the solution of interface failure was presented. The concept of `cohesive crack’ was adopted to describe the constitutive behavior of the cohesive interfacial layer. Related fundamental equations such as equilibrium equation, constitutive equations were presented. The behavior of a double shear beam bonded through cohesive layer was analytically calculated. The stable propagation of interface crack and process zone was investigated.     

帽型试样动态绝热剪切破坏演化分析

利用分离式霍普金森压杆加载Ta2钛合金扁平闭合帽形受迫剪切试样,结合数字图像相关法和“冻结”试样的微观金相观察,研究剪切区剪切应变的演化、绝热剪切带形成条件等。结果显示：受迫剪切试样在动态加载过程,剪切区剪切应变不断集中,形成绝热剪切带,裂纹沿绝热剪切带发展;随加载率提高,绝热剪切起始临界应变减小;进一步利用数字图像相关法DIC场应变分析及金相微观观测对比,利用卸载回复特性对绝热剪切带起始临界条件进行了讨论,计算的绝热剪切带起始时温升仅为86℃。材料软化可能不是绝热剪切带起始的控制条件,相反是由于绝热剪切带形成造成的应变高度集中发展导致温度急剧升高。