Experimental investigations on the dynamic behavior of a 2-DOF airfoil in the transitional Re number regime based on digital-image correlation measurements

The present paper investigates the fluid–structure interaction (FSI) of a wing with two degrees of freedom (DOF), i.e., pitch and heave, in the transitional Reynolds number regime. This 2-DOF setup marks a classic configuration in aeroelasticity to demonstrate flutter stability of wings. In the past, mainly analytic approaches have been developed to investigate this challenging problem under simplifying assumptions such as potential flow. Although the classical theory offers satisfying results for certain cases, modern numerical simulations based on fully coupled approaches, which are more generally applicable and powerful, are still rarely found. Thus, the aim of this paper is to provide appropriate experimental reference data for well-defined configurations under clear operating conditions. In a follow-up contribution these will be used to demonstrate the capability of modern simulation techniques to capture instantaneous physical phenomena such as flutter. The measurements in a wind tunnel are carried out based on digital-image correlation (DIC). The investigated setup consists of a straight wing using a symmetric NACA 0012 airfoil. For the experiments the model is mounted into a frame by means of bending and torsional springs imitating the elastic behavior of the wing. Three different configurations of the wing possessing a fixed elastic axis are considered. For this purpose, the center of gravity is shifted along the chord line of the airfoil influencing the flutter stability of the setup. Still air free-oscillation tests are used to determine characteristic properties of the unloaded system (e.g. mass moment of inertia and damping ratios) for one (pitch or heave) and two degrees (pitch and heave) of freedom. The investigations on the coupled 2-DOF system in the wind tunnel are performed in an overall chord Reynolds number range of $9.66\times 10^3\le \text{Re}\le 8.77\times 10^4$. The effect of the fluid-load induced damping is studied for the three configurations. Furthermore, the cases of limit-cycle oscillation (LCO) as well as diverging flutter motion of the wing are characterized in detail. In addition to the DIC measurements, hot-film measurements of the wake flow for the rigid and the oscillating airfoil are presented in order to distinguish effects originating from the flow and the structure.     

基于三维虚拟现实的互动实验教学系统

针对目前我国高等学校普遍存在实验设备不足、型号落后、难以更新换代跟上科技发展的现象,虚拟现实技术的应用为高校实验教学提供了一个良好的解决方案。本文简单介绍了虚拟现实技术的特点,通过对虚拟现实实验教学系统的详细分析,探讨了虚拟现实技术对实验教学的影响。     

基于LABVIEW的激光实验光路调节系统

针对当前大部分超短超强激光实验中真空光路调控效率低、操作方式繁琐等缺点,设计了一种基于LabVIEW软件开发平台的集成化实验光路调节系统来实现对光路高效便捷的调控。该系统由光斑位置采集单元、光斑位置调节单元和计算机等三部分构成,其设计思路是利用激光光斑映射在CCD上的空间位置,实现光路指向定位的反馈,根据反馈信息设计人机交互界面实现光路指向的调控。该系统成功实现多线程并行运行,并将不同型号不同通讯方式的多个位移台控制器集成于同一界面控制。实验证明,与常用的手动调节系统相比,该系统对实验光路的调控更方便快捷,调节效率更高。     

爆轰试验中高速摄影控制及闪光装置改进

研究爆轰试验高速摄影中,闪光灯和摄影机快门失灵引起试验失败问题,提出对试验操控装置和闪光灯电源改进措施。首先,在实验操控上增加防止仅雷管起爆的逻辑控制,并采用集中控制,分布检测设计;其次,在闪光氙灯电源中,采用伪火花开关和多节LC（电感-电容）脉冲形成线技术,解决氙灯存在的自闪、不引燃和光强不均。此外,还解决了装置研制中遇到的电磁干扰、同步引燃等问题。通过改进,有效地防止了爆轰试验中高速摄影光学影像丢失情况和底片曝光不均匀现象,介绍了主要元件、线路和系统、实验结果及研制过程。     

在线社交网络控制实验的现状与展望

在线社交网络已发展成为一个独特的电子生态系统,其应用深刻影响着人们生活的方方面面。由于在线社交网络特性复杂,分析在线社交网络形成和变化中的规律成为当前计算机科学、社会学和物理学的一项挑战。传统上,在线社交网络实证研究主要采用计算机辅助的被动数据获取和分析方式。近年来,在真实大规模在线社交网络上直接进行控制实验从而主动获取数据并开展分析研究的方式广受关注。评述了这一领域的研究进展,包括：社交网络控制实验的主要研究模式;控制实验方法在社交网络结构、信息传播、行为和心理学等领域取得的主要成果以及主要实验工具的适用条件和局限性。最后,展望了人工智能技术在社交网络控制实验中的应用潜力,分析了智能算法对降低实验成本和提高实验效率的作用。     

作图法研究物理实验数据处理中的线性回归问题

用作图的方法研究物理实验数据处理中的一元线性回归问题,通过作回归直线和标准差平行四边形,求出线性回归方程标准差和相关系数。     

基于模糊控制的计算机控制实验平台的设计

为加强计算机控制实验和自动控制理论实验的结合,提高教学实验水平,选择工业生产和科学实验中的重要物理量温度作为被控制量,而模糊控制是目前应用较为广泛、设计简单且在温度控制中取得了较好的控制效果的控制方法,为此开发了基于模糊控制的计算机控制实验平台。论文设计了基于PC机一单片机的分布式温度实时控制系统,根据温度控制系统的特点,给出了温度控制系统模糊控制器的实现方法,实验平台具有硬件透明、软件开放等特点,且模糊规则修改灵活方便,适合于学生实验使用。     

激光多脉冲探测的计算机模拟与实验研究

对激光多脉冲探测理论进行了分析,在考虑了影响探测的各种噪声及其分布特性的基础上,得到了激光多脉冲探测信噪比与脉冲积累次数的定量关系。利用计算机仿真模拟多脉冲探测,其结果与理论分析相符;在实验室条件下对多脉冲探测进行了研究,实验结果表明,在脉冲叠加数较少时,实验与理论符合得很好,当脉冲叠加数较多时,实验数据明显小于理想的数值,分析了出现这种偏差的原因及解决方案。激光多脉冲积累探测可以有效地提高激光探测的信噪比,应用积累探测的方式能有效地将激光探测的弱信号从强噪声背景中检测出来。     

A Global Optimization Algorithm for Multivariate Functions with Lipschitzian First Derivatives

In this paper we propose a new multi-dimensional methodto solve unconstrained global optimization problems with Lipschitzianfirst derivatives. The method is based on apartition scheme that subdivides the search domain into a set of hypercubesin the course of optimization. This partitioning is regulated by thedecision rule that provides evaluation of the "importance"of each generated hypercube and selection of some partition element to performthe next iteration. Sufficient conditions of global convergence for the newmethod are investigated. Results of numerical experiments are alsopresented.     

Accuracy assessment to applying 20-node solid elements to pressurized composite shells

A factorial analysis is conducted to explore the impact of five factors — aspect ratio, radius-to-thickness ratio, material anisotropy, fiber angle and integration order on the finite element accuracy, with regard to the application of 20-node isoparametric solid elements to clamped composite cylindrical shells subjected to internal pressure. The maximum radial displacement at the central cross-section is employed as the indicator of accuracy. Results from finite element methods were compared with closed-form solutions. Aspect ratio, radius-to- thickness ratio, and integration order are significant main effects as predicted for isotropic materials. Material anisotropy shows no significant main effect, while the fiber angle does have strong impact on the finite element accuracy. In addition to four influential main effects, some multiple-factor interactions are shown to have significant influences on the finite element accuracy. The analysis is limited to the linear elastic range.