基于离散元方法的沥青混合料虚拟断裂试验(英文)

为了深入研究沥青混合料开裂特性, 设计了基于沥青混合料二维数字试件的断裂虚拟试验. 在考虑混合料二维截面的集料数量级配和集料不规则形状的基础上, 通过生成程序建立了沥青混合料的二维虚拟试件; 运用离散元方法, 建立了混合料二维离散元模型, 并进行了虚拟的中点弯曲小梁断裂试验; 为了验证虚拟试验方法的正确性, 在实验室内进行了沥青混合料小梁的中点弯曲断裂试验. 室内实体试验与虚拟试验结果的比较发现, 虚拟断裂试验获得的混合料断裂强度与室内试验结果一致, 表明虚拟断裂试验可以作为混合料断裂性能分析的辅助手段.     

基于SCB试验的环氧沥青混合料断裂特性评估(英文)

运用J-积分与终极抗拉强度评估了环氧沥青混合料在-10℃和20℃的断裂特性, 共测试了60个不同切口深度的半圆弯曲试件. 结果表明, 环氧沥青混合料的半圆弯曲试验(SCB)结果复现性好; 由非切口试件的半圆弯曲试验与标准间接拉伸试验(IDT)所测得的环氧沥青混合料的抗拉强度, 其比值在1.4～1.7之间, 且SCB抗拉强度与切缝深度指数相关; 在20℃与-10℃试验条件下, 环氧沥青混合料具有比热塑性HMA高得多的临界J-积分值; 当温度由20℃降至-10℃时, 环氧沥青混合料的响应模式由延性变为脆性, 断裂能增加30%, 而临界J-积分值下降15%. 与热塑性HMA相比, 环氧沥青混合料的常温与低温抗裂性更好; 环氧沥青混合料低温起裂需要更高的能量, 但其裂纹扩展速度比常温时更快.     

《淮南子》许高二注相杂一书之历史探原

《淮南子》是一部重要的汉代典籍,许慎、高诱先后为之作注。在后来的流传过程中,许高二注相杂于一书。清代学者对许高二注何时相杂看法颇有分歧,甚至自相冲突。史志官私书目和文献征引材料表明,许高二注在宋代以前并行别传,杂于一书则是发生在北宋太宗至仁宗这百年之间,起因可能是缘自一场王宫大火。     

基于时域卷积盲信号分离的雷达干扰抑制算法

把卷积盲分离算法应用于雷达系统抗干扰中,提出一种新的雷达系统干扰抑制算法. 该算法在时域中对四阶累积量进行联合块对角化,以实现雷达信号和干扰信号的盲分离. 计算机仿真结果表明,在无噪及含噪情况下,该算法均可把卷积混合的雷达回波信号及干扰信号分离开来,且有很好的分离性能.     

基于核方法和高斯混合模型的手机上网时长统计分析及应用

从不同手机型号角度,分析上网时长的分布,并用核方法和高斯混合模型对手机上网时长数据进行建模和分析。实际数据分析表明,手机上网时长分布具有双峰现象,本文对此现象给出了合理解释。     

基于光谱混合分析的城市植被覆盖度与地表温度关系的研究

分别选择NDVI和光谱混合分析植被组分(VF)作为城市植被覆盖度指示因子,研究植被覆盖度与地表温度(LST)的相关关系.选择了一定数量的样本点,通过线性拟合的方法研究了NDVI及VF与LST的相关关系.研究结果表明,VF与LST之间的相关性比NDVI与LST之间相关性更好.研究表明,在城市LST研究中VF可以作为表征植被性质的参数.     

3D finite element analysis of the residual stresses in butt-welded plates with modeling of the electrode-movement

In this paper the residual stresses in a butt-welded plate of2.25Cr 1Mo has been analyzed using a 3D and transient finite element （FE） model. Also the effect of the welding-electrode speed has been studied using death and birth of FEs. For this purpose, a coupled thermo-mechanical FE solution has been used to obtain the temperature distribution and the resulting residual stresses. Also, the variations of the physical properties of the material with temperature have been taken into account. Results show that the residual stresses in the heat affected zone （HAZ） are maximum and change along the weld and also in the plate-thickness. It has been shown that use of the 3D and transient model will lead to more accurate and realistic results which are well compared with the experimental test data.     

Machining distortion prediction of aerospace monolithic components

To predict the distortion of aerospace monolithic components, a model is established to simulate the numerical control （NC） milling process using 3D finite element method （FEM）. In this model, the cutting layer is simplified firstly. Then, the models of cutting force and cutting temperature are established to gain the cutting loads, which are applied to the mesh model of the part. Finally, a prototype of machining simulation environment is developed to simulate the milling process of a spar. Key factors influencing the distortion, such as initial residual stress, cutting loads, fixture layout, cutting sequence, and tool path are considered all together. The total distortion of the spar is predicted and an experiment is conducted to validate the numerical results. It is found that the maximum discrepancy between the simulation results and experiment values is 19.0%.     

Finite particle method for kinematically indeterminate bar assemblies

This study presents a structural analysis algorithm called the finite particle method （FPM） for kinematically indeterminate bar assemblies. Different from the traditional analysis method, FPM is based on the combination of the vector mechanics and numerical calculations. It models the analyzed domain composed of finite particles. Newton＇s second law is adopted to describe the motions of all particles. A convected material flame and explicit time integration for the solution procedure is also adopted in this method. By using the FPM, there is no need to solve any nonlinear equations, to calculate the stiffness matrix or equilibrium matrix, which is very helpful in the analysis of kinematically indeterminate structures. The basic formulations for the space bar are derived, following its solution procedures for bar assemblies. Three numerical examples are analyzed using the FPM. Results obtained from both the straight pretension cable and the suspension cable assembly show that the FPM can produce a more accurate analysis result. The motion simulation of the four-bar space assembly demonstrates the capability of this method in the analysis ofkinematically indeterminate structures.     

Low-complexity multiplexer-based normal basis multiplier over GF(2m)

We present a new normal basis multiplication scheme using a multiplexer-based algorithm. In this algorithm, the proposed multiplier processes in parallel and has a multiplexer-based structure that uses MUX and XOR gates instead of AND and XOR gates. We show that our multiplier for type-1 and type-2 normal bases saves about 8% and 16%, respectively, in space complexity as compared to existing normal basis multipliers. Finally, the proposed architecture has regular and modular configurations and is well suited to VLSI implementations.