覆冰导线绕流的数值模拟

利用采用高阶有限差分的迎风格式,从探讨网格模型与计算结果之间的关系入手,通过数值计算模拟了新月形冰型的覆冰导线模型在不同攻角下的阻力系数、升力系数以及斯特鲁哈尔系数的变化规律,并与高雷诺数试验结果进行了对照分析。在一定程度上,数值结果反映了新月形冰型的覆冰导线模型气动力特性。     

恶意软件特征分析与危害防范

阐述了恶意软件的定义和基本特征,对我国网络法律法规的缺失和恶意软件泛滥的情况进行了调查与分析,从恶意软件的危害性和特征出发,总结了恶意软件泛滥的几个原因,并提出了一些防范恶意软件的基本方法。     

带Poisson跳的随机种群扩散系统半隐式欧拉方法的数值解

讨论了带Poisson跳的随机种群扩散系统,利用It公式、Burkholder-Davis-Gundy不等式、Gronwall引理及一些不等式,根据半隐式欧拉方法,证明了带Poisson跳的随机种群扩散系统数值解的收敛性.最后,通过数值算例对数值方法进行了说明.     

一类神经传导方程的修正的变网格有限元方法

研究了在神经传播过程中的一类非线性拟双曲方程的初边值问题．对二维情形应用常规变换，在常规的变网格有限元格式的基础上，提出了一种改进的变网格有限元格式，通过细致的分析和估计得到了最佳阶模误差估计结果，并使时间精度提高一阶．最后作了数值实验，说明方法是高效可行的．     

戈壁琵甲(鞘翅目:拟步甲科)生物学特性的研究

戈壁琵甲2年发生1代，世代不整齐，以成虫和不同龄期的幼虫越冬，成虫4月上旬至9月下旬产卵，卵期为8～12d．幼虫一般为12龄．幼虫期为1～1．5a．越冬幼虫于次年6月下旬至9月上旬化蛹．蛹前期为40～45d，蛹期为12～20d．羽化成虫后经280～300d性成熟，开始交配产卵，戈壁琵甲食性杂．不喜光．活动有明显的节律性．成虫具有利用防御腺进行自卫的特性，其防御腺分泌物可成为医学上的天然药物，该幼虫各项营养成分较高，是一种很有开发价值的昆虫资源。     

蓄滞洪区平面二维干河床洪水演进数值模拟

在地形较复杂的情况下,采用常用的处理干河床问题的方法有时会出现水流虚假流动的现象。本在洪水干河床演进模拟中提出了“水位平铺”假设进行处理,取得了比较好的模拟效果。模型建立过程中采用有限差分法的逆风格式离散控制方程,并用ADI方法求解代数方程组,模型计算速度快,节约计算内存,基本可以满足洪水实时预报要求。     

桂中坳陷东部下石炭统鹿寨组泥页岩有机地球化学特征

基于对桂中坳陷东部下石炭统鹿寨组泥页岩总有机碳含量(TOC)、有机质成熟度(Ro)、显微组分、饱和烃色谱-质谱等有机地球化学特征分析,发现其TOC主体2.0%,Ro为0.84%~2.95%,有机质类型属于Ⅱ1-Ⅱ2型。通过对比国内外主要页岩气盆地富有机质泥页岩有机地球化学特征和分析研究区页岩气保存条件,判断下石炭统鹿寨组泥页岩具有较好生烃潜力。在此基础上,分析了鹿寨组泥页岩的沉积环境和有机质来源,发现:Pr/Ph1,伽马蜡烷/αβC30霍烷比值为0.72~0.75,具有升霍烷系列,C27重排甾烷/C27规则甾烷比值为0.13~0.15,孕甾烷/C29-20R规则甾烷比值为0.03~0.04,研究区属于高咸度贫氧-缺氧的强还原环境;正构烷烃分布范围宽,C、N原子比为42.23~50.89,三环萜烷中C21、C23、C24呈倒"V"形分布,αβC30霍烷/∑C29甾烷比值为0.48~0.51,C29具有明显优势,伽马蜡烷指数平均值为0.370.2,不同显微组分在剖面上对TOC贡献率不同,判断鹿寨组泥页岩有机质来源多样,以高等植物和水生生物为主,顶部和底部层位有机质来源以低等细菌、藻类为主,具有较好的生烃潜力。     

改进型单晶炉提拉系统偏心平衡研究

随着光伏行业的快速发展, 对硅单晶的品质和长晶装备的稳定性的要求也不断提高。直拉法是生产硅单晶的主要方法,通过提高单晶炉副室的高度以扩大单晶硅的生产规模。由于副室高度的大幅增加,且单晶炉提拉头质心相对于旋转轴心有一定距离,对单晶炉整体稳定性有较大影响,从而降低了单晶硅的生产质量。针对此问题,对单晶炉建立可靠的力学分析模型,采用数值仿真方法,对单晶炉整体进行动力学响应分析,计算得到副室高度增加后的单晶炉工作时中钨丝绳下端晶棒的运动规律以及最大摆动幅度,为改进设计提供依据。数值仿真分析表明提高单晶炉副室高度后,提拉头较大的质心偏心是单晶炉提拉系统发生摆动的主要原因。在此基础上提出在提拉头上添加质心调节装置,通过控制系统调节可保证提拉头质心位置在旋转轴线上以降低提拉系统的摆动。     

On Physically Unacceptable Numerical Solutions Yielding Strong Chaotic Signals

Physically unacceptable chaotic numerical solutions of nonlinear circuits and systems are discussed in this paper. First, as an introduction, a simple example of a wrong choice of a numerical solver to deal with a second-order linear ordinary differential equation is presented. Then, the main result follows with the analysis of an ill-designed numerical approach to solve and analyze a particular nonlinear memristive circuit. The obtained trajectory of the numerical solution is unphysical (not acceptable), as it violates the presence of an invariant plane in the continuous systems. Such a poor outcome is then turned around, as we look at the unphysical numerical solution as a source of strong chaotic sequences. The 0–1 test for chaos and bifurcation diagrams are applied to prove that the unacceptable (from the continuous system point of view) numerical solutions are, in fact, useful chaotic sequences with possible applications in cryptography and the secure transmission of data.     

Nonlinear Modeling Study of Aerodynamic Characteristics of an X38-like Vehicle at Strong Viscous Interaction Regions

Strong viscous interaction and multiple flow regimes exist when vehicles fly at high altitude and high Mach number conditions. The Navier–Stokes(NS) solver is no longer applicable in the above situation. Instead, the direct simulation Monte Carlo (DSMC) method or Boltzmann model equation solvers are usually needed. However, they are computationally more expensive than the NS solver. Therefore, it is of great engineering value to establish the aerodynamic prediction model of vehicles at high altitude and high Mach number conditions. In this paper, the hypersonic aerodynamic characteristics of an X38-like vehicle in typical conditions from 70 km to 110 km are simulated using the unified gas kinetic scheme (UGKS), which is applicable for all flow regimes. The contributions of pressure and viscous stress on the force coefficients are analyzed. The viscous interaction parameters, Mach number, and angle of attack are used as independent variables, and the difference between the force coefficients calculated by UGKS and the Euler solver is used as a dependent variable to establish a nonlinear viscous interaction model between them in the range of 70–110 km. The evaluation of the model is completed using the correlation coefficient and the relative orthogonal distance. The conventional viscous interaction effect and rarefied effect are both taken into account in the model. The model can be used to quickly obtain the hypersonic aerodynamic characteristics of X38-like vehicle in a wide range, which is meaningful for engineering design.