含预置裂纹的CFRP层合板弯曲性能研究

分别对含有不同位置、角度和长度预置裂纹的T700/6240复合材料层合板进行三点弯曲实验并结合微观表征手段以研究不同裂纹参数对层合板弯曲性能和失效方式的影响,并建立裂纹长度与试样弯曲强度和模量之间的关系模型。利用ABAQUS有限元软件建立含有预置裂纹的复合材料层合板三点弯曲模型,对比验证有限元方法与实验结果的一致性。结果表明,含有不同参数预置裂纹层合板的弯曲强度和模量均小于完好试样,预置裂纹位置从层合板的上层移至下层,弯曲强度下降幅度由19. 10%减小至6. 24%,模量的下降幅度在11. 34%～12. 97%之间;裂纹角度的增加对弯曲强度没有趋势性影响,但会导致其弯曲模量不断降低,裂纹角度为90°时较完好试样分别降低了19. 10%和12. 97%;裂纹长度的增加导致弯曲强度和模量分别呈线性和三次曲线递减。有限元仿真计算结果与实验值对比的误差小于10%,验证了有限元方法的可靠性。     

CFRP层合板冲击后压缩失效分析数值模拟

复合材料层合板的损伤容限是复合材料结构设计的关键因素。针对碳纤维增强复合材料(CFRP)层合板低速冲击损伤和压缩破坏问题,本文基于连续损伤力学和粘结单元模型,在ABAQUS中对两种不同冲击能量下的层合板进行了低速冲击和冲击后压缩仿真分析,并对层内和层间损伤进行了研究,分析了层合板的冲击损伤与压缩失效行为,通过与试验结果进行对比,验证了该模型的有效性。研究结果表明:冲击损伤对层合板的剩余压缩强度有着重要影响,试件的破坏开始于冲击损伤区域,并逐渐扩展到层合板的边缘,压缩力快速下降,层合板最终失效。     

基于响应面法的CFRP层合板挖补修理结构的单目标优化

对于CFRP层合板挖补修理结构的优化问题,首先通过三维实体单元建立三维损伤累积模型并通过试验验证所建立的仿真模型的有效性,然后采用拉丁超立方试验设计方法和响应面法构建了拉伸强度代理模型,最后基于遗传算法和代理模型进行联合优化。研究结果表明:数值模型与仿真模型吻合度较好,误差在10%以内,表明所建立的有限元模型具有有效性。拉伸载荷下挖补结构的失效模式以胶层的剪切失效为主,胶层损伤起始于层合板和补片0°层对应的位置,然后向四周扩展,胶层失效后补片失去承载能力,母板继续承载并在最窄处断裂。最佳胶层厚度、挖补角度和旋转角度分别为0.1035 mm、2.5°和0°。与常规挖补结构相比,拉伸强度提高了12.57%。采用遗传算法对CFRP层合板挖补结构进行优化,对提高挖补结构的力学性能具有重要意义。     

有限元分析碳纤层合板铺层方式对行人头部保护的作用

使用ABAQUS有限元分析软件,按照GB/T 24500-2009规定建立了成人头部冲击器撞击碳纤层合板模型,探讨了9种铺层方式下,头部伤害指标HIC值与最大侵入量、撞击持续时间和冲击能量吸收之间的关系,并比较了层合板不同铺层角度对行人头部损伤的影响。结果表明,HIC值大小基本与最大侵入量、撞击持续时间和冲击能量吸收有一定的反比关系;铺设三种角度的层合板最有利于行人头部保护;45°方向铺层对降低HIC值和减小最大侵入量贡献最大。     

复合材料层合板冲击损伤剩余强度分析

民用飞机复合材料结构设计时必须考虑复合材料层合板的冲击损伤.通过试验测量和数值模拟两种方法分析碳纤维增强复合材料层合板低速冲击损伤后的剩余压缩强度,试验采用标准试验规范进行测量,数值模拟分析采用层内渐进损伤模型和层间Cohesive模型模拟分析层合板冲击损伤以及剩余压缩强度.数值模拟与试验结果对比表明,该数值模拟分析方...     

穿透裂纹对层合板拉伸性能的影响

对含3种不同方向穿透裂纹的层合板进行了拉伸试验研究,通过观测试验过程与断口分析,研究了含穿透裂纹层合板的失效行为。在此基础上,采用ABAQUS软件建立了含穿透裂纹层合板渐进损伤有限元分析模型,对其拉伸性能进行了分析,并对初始损伤与裂纹扩展路径进行了研究,讨论了裂纹形式对复合材料层合板剩余拉伸强度的影响。结果表明,初始损伤发生在裂纹尖端,损伤有沿垂直于载荷方向扩展的趋势。裂纹方向的变化对层合板的剩余强度有明显影响。     

玻璃纤维复合材料层合板冲击后的压缩强度

对不同厚度的二维编织环氧玻璃纤维层合板进行落锤冲击试验及冲击后压缩破坏试验,以研究低速冲击对复合材料层合板剩余压缩强度(CAI)的影响。用透光描影及热揭层方法对冲击损伤形式进行描述。讨论了损伤宽度、损伤面积与冲击能量及剩余压缩强度、模量间的关系,并建立有限元模型,采用开口等效及软化夹杂等分析方法对材料的冲击后压缩强度值进行估算。     

复合材料层合板损伤容限敏感性参数研究

本文针对碳纤维增强复合材料层合板冲击下的损伤容限参数敏感性进行分析.对复合材料层合板损伤容限的影响参数、纤维角度、铺层顺序、层合板厚度、冲击速度和冲击角度等进行冲击损伤仿真,采用蔡-吴强度准则评价层合板冲击的剩余强度,并对各参数影响的敏感性排序,确定纤维角度和铺层顺序为复合材料层合板冲击下损伤容限的敏感参数.     

复合材料加筋层合板准静态压痕实验研究及数值分析

利用ABAQUS有限元程序所建立了一种基于用户子程序USDFLD和Hashin强度准则的复合材料损伤计算模型,用该模型对复合材料加筋层合板在静压痕力作用下主要发生的纤维拉伸破坏、纤维微屈破坏、基体拉伸破坏、基体压缩破坏、层间拉伸破坏、层间压缩破坏这几种基本损伤模式进行分析。对复合材料加筋层合板在静压痕力作用下进行损伤全过程数值研究,利用该有限元模型预测复合材料层合板静压痕力作用下的荷载-位移曲线以及凹坑深度与静压痕力的关系曲线。数值仿真与实验结果吻合较好,表明该损伤模型方法的可行性。复合材料层合板加筋后拐点处的凹坑深度明显加大,达到0.84mm。通过对加筋板的刚度和强度失效规律的分析,为进一步的复合材料格栅加筋结构(如飞机结构中复合材料后压力框)的性能分析提供参考。     

修复对含分层损伤复合材料层合板振动特性的影响

本文工作是通过对含不同大小分层层合板结构分析,讨论拉伸和剪切修复刚度对含层间分层损伤复合材料层合板振动特性的影响.基于修补分层损伤结构变形特点,将含损层合板的基板、上子板和下子板采用Mindlin板单元离散,而损伤区修复效应以虚拟连接单元模拟,建立相应的有限元分析模型和计算方法.通过对含损层合板的振动分析,讨论并验证本文提出的修复分层损伤模拟连接单元模型的可能性和正确性,依据拉抻和剪切修复刚度对含损层合板固有频率的分别影响与综合影响,得到对分层损伤复合材料层合板修补的指导性原则.     

一种复合材料低速冲击性能的简化预计方法

低速冲击引起的分层损伤是层合板的主要损伤模式。对分层损伤进行数值模拟有着重要的工程价值,合理的假设有助于问题的简化,对于计算量和计算精度有着重要的影响。本文研究了层合复合材料分层损伤分析模型的建模方法,基于三个基本假设建立了分析模型,采用LS-DYNA显式算法对层合板的冲击响应和分层损伤进行了计算,计算结果与实验结果的一致性证明了该方法的正确性。     

Experimental and Numerical Investigations of Honeycomb Sandwich Composite Panels With Open-hole Damage and Scarf Repair Subjected to Compressive Loads

The mechanical analysis of adhesive repair of honeycomb sandwich composite plate is more complicated than that of the laminated plate repair, because not only the laminated damage, but also the honeycomb buckling should be considered. Experimental and numerical investigations are carried out to understand the damage propagation and ultimate strength of both open-hole and repair plates under compressive load. The results of numerical models are verified by experimental data and they are found in good agreement. It is revealed from the results that the strength of open-hole plate is about 34% of the strength of intact plate, while the strength of repair plate could resume to 76% of that of intact plate after the repair process. It is found that the structure strength increases as the scarf repair angle decreases due to the decline of shear stress in the adhesive. We also present the optimum ply sequence and the optimum number of overlays in considering the improvement of structure strength. This research will be useful in improving the design and analysis techniques for scarf patch repair of sandwich structures.     

Evaluation of surface energy of solid polymers using different models

In the present work, contact angles formed by drops of diethylene glycol, ethylene glycol, formamide, diiodomethane, water, and mercury on a film of polypropylene (PP), on plates of polystyrene (PS), and on plates of a liquid crystalline polymer (LCP) were measured at 20°C. Then the surface energies of those polymers were evaluated using the following three different methods: harmonic mean equation and geometric mean equation, using the values of the different pairs of contact angles obtained here; and Neumann's equation, using the different values of contact angles obtained here. It was shown that the values of surface energy generated by these three methods depend on the choice of liquids used for contact angle measurements, except when a pair of any liquid with diiodomethane was used. Most likely, this is due to the difference of polarity between diiodomethane and the other liquids at the temperature of 20°C. The critical surface tensions of those polymers were also evaluated at room temperature according to the methods of Zisman and Saito using the values of contact angles obtained here. The values of critical surface tension for each polymer obtained according to the method of Zisman and Saito corroborated the results of surface energy found using the geometric mean and Neumann's equations. The values of surface energy of polystyrene obtained at 20°C were also used to evaluate the surface tension of the same material at higher temperatures and compared to the experimental values obtained with a pendant drop apparatus. The calculated values of surface tension corroborated the experimental ones only if the pair of liquids used to evaluate the surface energy of the polymers at room temperature contained diiodomethane. © 2000 John Wiley & Sons, Inc. J Appl Polym Sci 76: 1831–1845, 2000     

碳纤维增强铝合金层合板拉伸性能研究

采用试验方法与理论分析相结合,对两种不同纤维铺层结构的碳纤维增强铝合金层合板(CARALL)开孔前后的拉伸性能进行了比较研究,得出了开孔前后不同纤维铺层结构的层合板拉伸性能变化规律,并给出了作为拉伸构件的碳纤维铺层结构建议,提出了应用金属体积分数理论和点应力准则预测层合板开孔前后拉伸性能的方法。     

碳纤维复合材料曲梁冲击后四点弯曲强度及损伤失效模式研究

通过四点弯曲试验和落锤冲击试验,研究了复合材料层合曲梁冲击前后四点弯曲强度及其破坏模式。不仅通过超声C扫描分析了不同内径复合材料层合曲梁试件冲击后的损伤特征,而且分析了冲击损伤对层合曲梁强度及层间最大应力的影响;同时,通过数字散斑相关方法得到复合材料层合曲梁在四点弯曲载荷作用下的变形场以及失效模式。研究结果将为复合材料层合曲梁在飞行器结构中的应用提供有价值的实验依据。     

Significance of Peel Test Speed on Interface Strength in Cohesive Zone Modeling

The analysis of the experimental peel test data for obtaining the adhesion fracture energy of an adhesively laminated polymer to the sheet metal surface is considered. The experimental results of the 180° peel test on two types of polymer laminated sheet metal at three different peel speeds are analyzed by two methodological approaches in cohesive zone modeling. These approaches are linear-elastic stiffness approach and critical maximum stress approach. Comparing the results of these two approaches reveals the significance of the peel test speed on the interface strength determination for cohesive zone modeling. It is concluded that a “reference” peel speed may exist at which the interface strength is equal to the yield strength of the peel arm material. A constitutive equation has been proposed which relates the interface strength to the peel test velocity by using the reference peel speed and its corresponding peel arm yield strength.     

THE INFLUENCE OF POLARIZATION ON THE MICROWAVE DRYING PROCESS OF SHELLED CORN

In this paper the effect of electromagnetic polarization of the microwave field on drying of shelled corn was analyzed. The drying process was investigated in a microwave field of 2.45 GHz. A number of corn kernels with the same orientation were stocked on plastic plates and these plates with corn kernels on their surfaces were fixed to each other, creating the corn matrixes. Plastic plates and glue used to the experiments were inert, related to the applied microwave power. By rotating test materials the influence of different polarization angles of electromagnetic field could be registered. Furthermore, setting test material in different positions the effect of distance between the antenna and the corn matrix were observed

The experiments carried out showed that in moist crops placed in microwave field ion polarization is dominant and the drying rate depends on relationship between the electric field strength vector and the overall moisture gradient in the kernel.     

THE INFLUENCE OF POLARIZATION ON THE MICROWAVE DRYING PROCESS OF SHELLED CORN

ABSTRACT

In this paper the effect of electromagnetic polarization of the microwave field on drying of shelled corn was analyzed. The drying process was investigated in a microwave field of 2.45 GHz. A number of corn kernels with the same orientation were stocked on plastic plates and these plates with corn kernels on their surfaces were fixed to each other, creating the corn matrixes. Plastic plates and glue used to the experiments were inert, related to the applied microwave power. By rotating test materials the influence of different polarization angles of electromagnetic field could be registered. Furthermore, setting test material in different positions the effect of distance between the antenna and the corn matrix were observed

The experiments carried out showed that in moist crops placed in microwave field ion polarization is dominant and the drying rate depends on relationship between the electric field strength vector and the overall moisture gradient in the kernel.     

复合材料胶接修补结构疲劳性能的数值和试验研究

为研究室温下复合材料胶接修补结构的疲劳性能,以三维渐进损伤理论为基础,创建了复合材料胶接修补模型,利用材料损伤判断子程序实现对修补结构的静拉伸失效载荷及剩余强度的预测分析,并进行了相关试验的对比分析。采用5种不同尺寸的圆形补片来评价修补效果,并利用超景深仪对修补试件的疲劳损伤扩展模式进行微观测量。结果表明:静载拉伸中,尺寸为3.5r的修补结构承载能力最好;疲劳循环中,尺寸为2.5r的修补结构剩余强度提升效果最好;疲劳载荷下,当循环次数较低时,修补结构的主要损伤为基体开裂,而随着循环次数的增大,主要损伤为纤维断裂。