Sound insulation performance of plates with interconnected distributed piezoelectric patches

This paper deals with the sound insulation performance of a thin plate with intercon-nected distributed piezoelectric patches. Piezoelectric patches are periodically bonded on the sur-faces of the plate in a collocated fashion, and are interconnected via an inductive circuit network. This piezoelectric system is termed as piezo-electromechanical (PEM) plate in the paper. Homogenization methods are involved under a sub-wavelength assumption to analytically develop the dynamical equations for the PEM plate. The dispersion relationships and energy densities of the wave modes propagating in the PEM plate are studied;the sub-wavelength assumption is verified for the simulations in this paper. The coincidence frequency of the PEM plate is researched, and results show that the coincidence frequency of the PEM plate will disappear at certain circum-stances;mathematical and physical explanations are made for this phenomenon. The disappearance of the coincidence frequency is used to optimize the value of inductance, for the purpose of improv-ing the sound transmission loss of the PEM plate.     

一种验证科氏加速度存在的实验装置及其动力学分析

科氏加速度是理论力学中公认的教学重点和难点,如何将科氏加速度形象地展示出来一直是学者与高校老师追求的目标。针对这一知识点,结合地球仪的外形,巧妙地实现了小球在科氏地球仪上旋转运动和直线运动的完美结合。根据科氏加速度理论,设计转速可调的旋转平台,在平台上设置能实现不同速度的直线运动装置,小球在旋转平台上作直线运动,从而受到科氏力的作用。初始状态时,安装在运动装置内的钢球处于平衡状态;工作时,由于科氏力的作用,钢球压迫弹簧,弹簧发生变形,利用滑轮、引线和位移补偿丝杆组成的传递机构,将弹簧变形量传递到显示装置,从而显示科氏加速度的存在。与现有科氏加速度验证实验装置所不同的是,此装置结构新颖,能吸引学生深入理解和掌握科氏加速度的概念。     

临近空间高超声速目标滑跃式轨迹Sine-AIMM跟踪算法

针对单一的Sine模型算法无法与临近空间高超声速目标滑跃式轨迹准确匹配,现有的交互多模型(IMM)算法跟踪效果也不够理想的问题,提出一种基于多重贝叶斯准则的自适应交互式多Sine模型(Sine-AIMM)临近空间高超声速滑跃式目标跟踪算法.算法采用多个Sine模型对滑跃式轨迹进行匹配,并利用多重贝叶斯准则在线调整各模型...     

冷却塔群塔干扰条件下脉动风压分布模式

冷却塔群塔为常见的群体建筑物组合形式,存在复杂的塔群干扰效应.传统的群塔干扰效应研究通常面向塔筒等效静风荷载,忽略了群塔组合对于脉动风压分布模式干扰效应的量化研究.为了研究群塔组合条件下脉动风压的干扰分布模式,选取具备多种气动干扰特点的八塔组合矩形布置方案为研究对象,对群塔进行刚性模型同步测压风洞试验,获取了不同风向角...     

乘务类学生英语课程教学方法实证探析

通过问卷调查探析乘务类本科生对交际和非交际教学法及活动的认识和态度,旨在研究一种可以有效提高英语教学质量的方法.结果表明乘务类学生对交际教学活动和非交际教学活动都有偏好,因此对于此类学生更为有效的教学方法就是采取折中的综合性教学法.     

Evaluation of the Terrestrial Albedo Applied to Some Scientific Missions

Using the Earth albedo model and the orbital dynamics model developed as part of the First Look Project (Fast Initial In-Orbit Identification of Scientific Satellites) the terrestrial albedo is evaluated considering the orbits of some scientific missions as Gravity Probe B, MICROSCOPE and STEP. The model of the Earth albedo is based on the reflectivity data measured by NASA’s Earth Probe satellite, which is part of the TOMS project (Total Ozone Mapping Spectrometer). The reflectivity data are available daily, on line at the TOMS website, and they fluctuate because of changes in clouds and ice coverage and seasonal changes. The data resolution partitions the Earth surface into a number of cells. The incident irradiance on each cell is used to calculate total radiant flux from the cell. With the radiant flux from each cell, the irradiance at the satellite is calculated.     

大型双曲冷却塔表面脉动风压随机特性——风压极值探讨

针对风压信号呈现的非高斯特性和传统极限估计方法的局限,首次提出基于保证率和相关性的极值估计方法——全概率迭代法进行冷却塔表面脉动风荷载极值分析,并和传统的峰值因子法及改进的Sadek-Simiu法计算结果进行对比验证。结果表明：全概率迭代法避开了对随机过程的高斯分布假定,相比传统的极值估计方法其结果更加真实可靠;表达风压极值中脉动分量的峰值因子数值沿着环向和子午向变化显著,如取为同一数值则偏于危险或过于保守;采用全概率迭代法得到的表面风压系数极值分布曲线与规范取值相比,迎风面和负压峰值区域极值偏小,背风区域极值偏大,且最小值对应角度相差约10°。     

用于直升机现场计量的低频振动校准技术

本文面向直升机健康与使用监测系统(HUMS)的现场计量保障需求,针对其中振动传感器在低频段尚无法实现现场校准的现状,提出了基于直线电机驱动技术的便携式低频振动校准技术方案。该方案利用高精度直线电机构造低频标准振动源,采用稳定性高的石英挠性加速度计作为标准加速度计,具有体积小、精度高、现场环境适应性好的特点,非常适用直升机HUMS的现场计量保障。根据不确定度评估结果,该方案能够实现0.5Hz～20Hz频率范围,0.01m/s~2～20m/s~2加速度范围内不超过1%的校准不确定度(k=2)。     

《诗经》中女性生命价值的解读

中国的伦理文化中,对母性的塑造一方面是对"女色"的危害进行严惩,另一方面是对女性进行引导,使她们能够按照指定的方向行进,最终使所有的女性都安于贤妻良母的价值规范。透过《诗经》及后世对《诗经》的解读即可看出男性对女性的价值期待。     

Decision-making of Aircraft Optimum Configuration Utilizing Multidimensional Game Theory

As multi-discipline coupling and components interference often affect the aircraft configuration decision-making and analysis during conceptual design process, this article presents an approach of multidimensional game theory based on aircraft components to deal with this problem. The idea is that the configuration decision-making process is regarded as the game for different disciplines and technologies, and the aircraft components are players. The payoff function with highest total gain means that according to the game protocols and multidimensional theory, the optimal aircraft configuration within the strategy set will be chosen. The decision-making model is applied to conceptual design process of the high altitude long endurance (HALE) unmanned aerial vehicle (UAV) based on the assessment of technological risk. The obtained optimum configuration is quite consistent with the current HALE UAV development trends. Thus, taking into account the coupling and interference factors, the multidimensional gaming model based on aircraft components will be an effective analysis method in the decision-making process of aircraft optimum configuration.