填充硅橡胶的泡沫铝复合材料的力学性能

用渗流法向开孔泡沫铝-硅合金和泡沫纯铝中充填硅橡胶获得含硅橡胶的泡沫材料, 在材料试验机和SHPB上对含硅橡胶的复合材料进行动态与准静态压缩实验。实验结果表明:含硅橡胶的泡沫复合材料只有弹性段和塑性段两个阶段,具有更高的应变率敏感性,其应力-应变曲线抖动幅度比较大。     

准一维应变下Al2O3陶瓷动态压缩失效的实验研究

为了考察Al2O3陶瓷准一维应变下的力学性能,采用LY12铝套筒和45钢套筒对陶瓷试样进行了环向约束,在准静态和动态下分别进行了压缩实验,得到了材料的应力-应变曲线。实验结果表明,Al2O3陶瓷的轴向压缩强度基本上随围压的增大而增大,动态压缩加载下的轴向压缩强度随应变率增大而增大。Al2O3陶瓷在准一维应变下的破坏形式为裂纹破坏,准静态的脆性失效行为可以用Mohr-Coulomb失效准则来描述。     

空心微珠/Al复合材料的动态压缩力学性能和吸能特性

利用分离式霍普金森压杆（split Hopkinson pressure bar,SHPB）系统对空心微珠体积分数为0.4的空心微珠/1199Al复合泡沫在1 700~2 900s-1应变率范围内的动态压缩力学性能、吸能性能进行了研究,还利用SEM扫描电镜对压缩试件断口进行微观组织分析,与准静态条件下材料的压缩力学性能及压缩变形机制进行了对比。结果表明,空心微珠/1199Al复合泡沫是一种应变率敏感材料,与准静态结果相比,在高应变率下复合材料的流动应力和塑性应变有明显的增大,应变率硬化效应对复合材料的流动应力的影响明显大于应变硬化的影响。复合材料的准静态和动态压缩变形机制存在一定差异,动态载荷作用下,空心微珠/1199Al复合泡沫内部空心微珠的压缩和基体材料的充填同时发生,组分之间具有良好的协调变形能力。     

铝合金LC4和LY12CZ应变率相关力学性能的实验研究

对国产铝合金LC4和LY12CZ进行了准静态和动态拉伸、压缩试验研究。应变率范围从2×10(-4)～1.4×10~3s~(-1)。实验表明:LC4和LY12CZ都是应变率不敏感材料,同时发现它们的压缩应力应变曲线高于拉伸应力应变曲线。本文根据实验结果分别建立起该材料的本构方程。     

干、湿木材的动态力学性能及破坏机制研究

通过Hopkinson压杆实验研究了干、湿桉木在较高应变率下的应力-应变曲线,力学性能及破坏机制,并同准静态压缩实验的结果进行了比较．冲击压缩载荷作用下,干、湿桉木的破坏形式明显不同：干桉木纤维发生屈曲、坍塌,表现出应变率效应;湿桉木纤维束在水的作用下,沿轴向相互分离、溃散,较干按木表现出更明显的应变率效应,应力应变曲线的平台段出现尖峰．     

不同应变率下蓝宝石透明陶瓷玻璃的力学响应

蓝宝石（A1₂O₃）是透明陶瓷玻璃,它相较传统陶瓷（A1₂O₃）有优良的透光性,而且保留了陶瓷优良的力学性能。利用电子拉伸机和分离式霍普金森杆设备对试样进行准静态应变率为(10?4、10?3、10?2 s?1)和4种动态应变率(850、1 100、1 300、1 450 s?1)下的单轴压缩力学行为,用高速摄像机记录了蓝宝石透明陶瓷玻璃试样在准静态和动态压缩下的破坏过程。实验结果表明:从加载过程中的应力应变曲线是由加载段和失效段组成的,该材料是典型的脆性材料,并且有明显的应变率效应,随着应变率的提高,蓝宝石透明陶瓷玻璃的抗压强度也会提高;准静态和动态压缩下蓝宝石透明陶瓷玻璃都是在宏观裂纹扩展作用下失效破坏。通过分析不同应变率下蓝宝石透明陶瓷玻璃的破坏过程,分析得到该材料的失效是在加载的过程中,在蓝宝石透明陶瓷玻璃承载能力最低的区域出现裂纹源,然后裂纹成形并沿着加载方向扩展,然后裂纹之间相互交错,最终达到饱和状态破坏失效;在高应变率下,极短的时间内产生多处裂纹源,需要更大的能量去使裂纹成形、扩展,宏观上就表现为应变率效应。     

准静态压缩应力-应变曲线测量方法的探索

本文介绍了用应变片直接测量材料的准静态应力-应变曲线的试验研究。在MTS810材料试验机上分别对93W、G50、砂浆等几种材料进行了准静态压缩试验。由于仪器的系统误差不能由MTSCod规准确的得到材料的真实的弹性变形。为此在试件的中部贴应变片得到材料的弹性变形,塑性变形仍旧由MTSCod规记录,从而得到试样的真实的应变,准确获得准静态压缩应力-应变曲线。试验结果表明:在试件中部贴应变片的方法能够准确得到该材料的杨氏模量;在试件两端垫块的刀口上安置Cod规可得到材料的应力应变曲线。两者的合理组合即可得到准确而完整的准静态压缩应力-应变曲线。试验中还发现准静态实验中试件的断面加工不平,偏心压缩等都会影响E的准确测量。     

一种碳纤维织物增强复合材料应变率相关的各向异性强度准则

为了获得一种碳纤维二维正交平纹机织布增强树脂基复合材料在一维应变状态下的强度准则,在已完成的准静态和动态压缩实验的基础上,拟合出了单轴压缩下三个主方向上的计及应变率的应力-应变关系式,进而得到初始屈服应力和压缩破坏强度与应变率相关性表达式。依据该表达式,得到了该复合材料在一维应变下考虑应变率效应的Tsai-Hill屈服强度和破坏强度准则方程。通过计算,考察了Tsai-Hill屈服强度和破坏强度准则随应变率的变化规律。结果表明,本文中研究的复合材料的强度性能,不但存在应变率效应,而且这种效应是各向异性的。     

高应变率下ZrB2-SiC陶瓷复合材料压缩力学性能实验研究

采用分离式霍普金森压杆装置,测试了高应变率下ZrB2-20%SiC陶瓷复合材料的动态压缩力学性能,应变率范围为900s^-1~3000s^-1。结果表明:ZrB2-20%SiC陶瓷复合材料的动态压缩强度与临界应变均随应变率的增大而增加,2950s^-1时压缩强度与临界应变比981s^-1时分别增大了88.72%和148.85%;应变率对ZrB2-20%SiC陶瓷复合材料的动态压缩应力-应变曲线与破坏机理影响显著,应变率为1134s^-1时,ZrB2-20%SiC陶瓷复合材料破坏模式以裂纹扩展为主,应变率为2861s^-1时,多裂纹扩展为该材料的主要破坏机理;应变率越高,试件的损伤程度越大,压缩试件碎片尺寸越小,压缩应力-应变曲线的非线性越明显。     

硬质聚氨酯泡沫力学特性的静水压力加载实验方法研究

泡沫材料在多轴载荷下的力学性能是工程中非常关心的问题。利用土壤的三轴压缩试验装置,通过试验方法的改进,提出了一种体应变测定和修正的方法,对硬质聚氨酯泡沫材料的静水压力特性进行了研究,得到了一些有价值的数据和结论。研究表明:在准静态静水压加载条件下,该材料的应力-应变曲线明显地分为弹性段、塑性段和压实段,且屈服强度比单向压缩时略大、压实应变略小。最后通过不同高度的试样对比试验,对聚氨酯泡沫材料的不均匀变形和弯曲的原因进行了分析和比较,指出了试验时应该注意的问题。     

玻纤增强复合材料高应变率拉伸实验研究

利用爆炸膨胀环实验技术,对玻璃纤维增强复合材料(GFRC)进行了高应变率(104s-1)下力学性能研究。实验中使用铜丝汽化引爆装药的方法对驱动环进行能量加载,并采用激光速度干涉仪(VISAR)测量试样环自由膨胀的质点速度,实现了玻璃纤维增强复合材料在104应变率下的一维拉伸破坏,并获取了该材料的速度时间曲线。经过计算得到了材料的应力应变关系,最后与该材料在准静态下、中高应变率下实验得到的数据进行了比较。     

Mechanical behavior of metals under tension- compression loading at high strain rate

By using a new technique based on a split Hopkinson pressure bar method, a sequenced reverse test (quasi-static tensile prestress, followed by dynamic compression and then followed by dynamic tension) at high strain rate was performed and tension-compression stress-strain relations were derived by using one-dimensional stress wave analysis. Three materials, 2017 aluminium alloy, 0.45% carbon steel, and pure aluminium, were investigated at low and high strain rates, and the strain rate effect on the reverse loading stress-strain curves was compared to that on the loading stress-strain curves. It was found that reduction of yield stress is always associated with load reversals, and the strain rate effect on the reverse loading (tension) is almost the same as that during loading (compression) at higher values of reverse deformation.     

准三维针刺C_f/SiC复合材料室温层向动态压缩力学行为的实验研究

为了研究应变率对准三维针刺碳纤维增韧的碳化硅复合材料(Cf/SiC)层向压缩力学性能的影响,本文利用分离式Hopkinson压杆装置对三维针刺Cf/SiC复合材料进行了应变率为10-4至6.5×103s-1的单轴压缩力学性能测试。实验结果表明,由于材料缺陷,其动态压缩强度分布遵循Weibull分布。破坏时,材料并未表现出典型的脆性破坏,而是在应力达到压缩强度后经历了较大的伪塑性变形才最终破坏。这表明三维针刺Cf/SiC复合材料沿厚度方向针刺的碳纤维有助于提高材料的韧性。同时,材料的压缩强度随应变率的升高显著增大,并与对数应变率近似成线性关系。借助光学显微镜和扫描电镜对压缩断口的观察表明:材料的失效模式随着应变率变化而发生改变。在准静态下,材料主要表现为剪切和分层破坏,而在高应变率下,则主要表现为劈裂。     

酚醛层压材料的冲击力学行为及本构模型

为了研究酚醛层压材料的冲击力学行为并获得本构模型,利用万能试验机和整形修正的分离式霍普金森压杆(SHPB)装置,对材料试样进行了应变率范围为10-3~103 s-1的单轴压缩实验,得到了不同加载应变率下的应力应变曲线,对其在准静态、动态载荷下的压缩破坏机理进行了初步探讨。结果表明,酚醛层压材料具有较强的应变率效应,与准静态(1.67×10-3 s-1)时相比,在动态载荷(7×102 s-1)下,峰值应力增加了约10倍;破坏应变减少了约一半;在准静态和动态加载条件下试样力学性能的差异是由于纤维基体界面特性以及不同应变率下破坏模式的不同;采用朱-王-唐本构方程描述了酚醛层压材料力学行为,拟合得到了本构方程的系数,在加载过程中,理论计算值与实验结果吻合较好。     

Dynamic compressive behavior of thick composite materials

The effect of strain rate on the compressive behavior of thick carbon/epoxy composite materials was investigated. Falling weight impact and split Hopkinson pressure bar systems were developed for dynamic characterization of composite materials in compression at strain rates up to 2000 s^–1. Strain rates below 10 s^–1 were generated using a servohydraulic testing machine. Strain rates between 10 s^–1 and 500 s^–1 were generated using the drop tower apparatus. Strain rates above 500 s^–1 were generated using the split Hopkinson pressure bar. Unidirectional carbon/epoxy laminates (IM6G/3501-6) loaded in the longitudinal and transverse directions, and cross-ply laminates were characterized. The 90-deg properties, which are governed by the matrix, show an increase in modulus and strength over the static values but no significant change in ultimate strain. The 0-deg and cross-ply laminates show higher strength and ultimte strain values as the strain rate increases, whereas the modulus increnases only slightly over the static value. The increase in strength and ultimate strain observed may be related to the shear behavior of the composite and the change in failure modes. In all cases, the dynamic stress-strain curves stiffen as the strain rate increases. The stiffening is lowest in the longitudinal direction and highest in the transverse direction.     

PMMA材料的动态压缩力学特性及应变率相关本构模型研究

利用INSTRON万能试验机和分离式Hopkinson压杆(SHPB)对PMMA试件在较宽应变率范围内进行了单轴压缩实验,研究加载应变率对PMMA材料力学性能的影响.利用扫描电子显微镜对回收的试样进行了显微观察,重点分析不同加载应变率下PMMA的微观损伤破坏模式.结果表明:随着应变率的增大,PMMA的流动应力显著地增加,且冲击加载条件下,峰值应力的应变率敏感性明显高于准静态;在准静态加载条件下,PMMA试样呈现明显的延性破坏特征,在动态加载条件下则表现为脆性破坏.最后,对PMMA材料的ZWT粘弹性本构模型参数进行了拟合,拟合结果与实验结果吻合较好,表明该本构模型能够较好地描述较宽应变率范围内PMMA材料的应力应变关系.     

Strain-Rate-Dependent Failure of a Toughened Matrix Composite

The strain-rate-dependent behavior of a toughened matrix composite (IM7/8552) was characterized under quasi-static and dynamic loading conditions. Unidirectional and off-axis composite specimens were tested at strain rates ranging from 10^?4 to 10³ s^?1 using a servo-hydraulic testing machine and split Hopkinson pressure bar apparatus. The nonlinear response and failure were analyzed and evaluated based on classical failure criteria and the Northwestern (NU) failure theory. The predictive NU theory was shown to be in excellent agreement with experimental results and to accurately predict the strain-rate-dependent failure of the composite system based on measured average lamina properties.     

Characterization of Anisotropic Polymeric Foam Under Static and Dynamic Loading

An orthotropic polymeric foam with transverse isotropy (Divinycell H250) used in composite sandwich structures was characterized at various strain rates. Uniaxial experiments were conducted along principal material axes as well as along off-axis directions under tension, compression, and shear to determine engineering constants, such as Young??s and shear moduli. Uniaxial strain experiments were conducted to determine mathematical stiffness constants, i. e., C _ij . An optimum specimen aspect ratio for these tests was selected by means of finite element analysis. Quasi-static and intermediate strain rate tests were conducted in a servo-hydraulic testing machine. High strain rate tests were conducted using a split Hopkinson Pressure Bar system built for the purpose using polymeric (polycarbonate) bars. The polycarbonate material has an impedance that is closer to that of foam than metals and results in lower noise to signal ratios and longer loading pulses. It was determined by analysis and verified experimentally that the loading pulses applied, propagated along the polycarbonate rods at nearly constant phase velocity with very low attenuation and dispersion. Material properties of the foam were obtained at three strain rates, quasi-static (10^?4 s^?1), intermediate (1 s^?1), and high (10³ s^?1) strain rates. A simple model proposed for the Young??s modulus of the foam was in very good agreement with the present and published experimental results.