AD－200轻型飞机舱内噪声源传声途径识别

为使建立在双传声器互谱声强基础上的识别方法在飞机上应用,进行了模拟测量。分别以带号筒的扬声器和激振器模拟空气传声和结构传声。模拟测量结果表明：空气传声和结构传声平均声强级识别值的误差分别为１．７ｄＢ（Ａ）和０．４ｄＢ（Ａ）,满足工程应用要求。在此基础上,对ＡＤ－２００轻型飞机在发动机工作下进行了地面测量。结果表明机舱内噪声主要来自座舱后隔板的空气传声。     

太阳风中低频离子静电孤波

本文给出在太阳风超声速流动条件下,离子静电孤波的传播特性,结果与Helios1,2卫星观测的静电离子噪声做了比较。离子声波扰动的非线性发展使太阳风等离子体呈规则的小尺度起伏,离子声波在马赫锥外传播,因此理论预言密度起伏不沿着太阳风速度方向,而是在横向方向.      

复杂动态系统实时仿真模型自动生成

提出了一种表示复杂动态系统数学模型的分层结构,探讨了模型变量与参数在实时仿真程序中的引用－赋值关系,提出了一个既包含了模型的数学特征,又包含了模型实时运行所需的信息的实时仿真模型分层结构。在此基础上设计了一个实时仿真模型库及实时仿真模型自动生成系统。     

低雷达散射目标的RCS分析与求解

利用Ｃ－Ｒ样条对目标进行建模和求解爬行波短程线,通过ＧＲＥＣＯ与爬行波混合法求解低散射目标后向ＲＣＳ。获得令人满意的结果。     

运载火箭起飞噪声环境缩比模型试验方法

基于相似理论建立缩比模型试验相似准则,提出了火箭发动机喷流声场试验预示方法的流程。通过缩比模型系留点火试验,根据几何相似、喷流参数相似、发射环境相似来预示起飞噪声环境,在国内首次给出了运载火箭表面的噪声环境的空间相关特性,结果表明预测结果与遥测数据之差小于1.5 dB,校验了缩比模型方法的有效性。缩比模型方法对于我国新一代运载火箭的起飞噪声环境预示、噪声载荷设计、地面试验具有重要意义。     

30cm离子推力器在轨环境下的工作点及热控措施研究

栅极间距变化是影响离子推力器在轨环境下从冷态条件正常点火启动的重要因素,同时也决定了离子推力器的在轨工作时机和热控实施策略。本文采用有限元仿真与地面热平衡试验验证相结合的方法,建立起30cm离子推力器有限元分析模型并进行了模型校验,之后对离子推力器在轨受太阳光照影响的栅极温度场分布和间距变化,以及推力器在5kW工况下的三个典型温度点所对应的栅极间距变化进行了仿真分析,最后考虑了主动热控干预对推力器最恶劣工作点的栅极间距变化影响。结果显示：纯太阳光照影响下的栅极组件存在周期性温度变化,栅极最大温差可达到100℃,栅间距缩小量在0.06mm~0.16mm范围内波动;在太阳光照基础上实施60W的主动热控后,栅极最大温差降低至60℃,栅间距缩小量波动范围则变为0~0.03mm;栅极最高温度点和最低温度点分别是推力器冷态启动最容易和最困难的两个工作时机点,两点所对应的启动后屏栅和加速栅最小间距分别为0.22mm和0.04mm;在10W、70W和120W的热控加热功率下,从最低温度点启动后的屏栅和加速栅最小间距分别为0.06mm、0.20mm和0.29mm;采取主动热控措施能够有效降低推力器工作过程中的栅极热形变位移峰值,且加热功率为120W即温控点温度为50℃的主动热控可以满足30cm离子推力器在轨冷态启动时的0.25mm安全栅极间距要求。     

A self-similar solution of a curved shock wave and its time-dependent force variation for a starting flat plate airfoil in supersonic flow

The problem of aeroelasticity and maneuvering of command surface and gust wing interaction involves a starting flow period which can be seen as the flow of an airfoil attaining suddenly an angle of attack. In the linear or nonlinear case, compressive Mach or shock waves are generated on the windward side and expansive Mach or rarefaction waves are generated on the leeward side. On each side, these waves are composed of an oblique steady state wave, a vertically-moving one-dimensional unsteady wave, and a secondary wave resulting from the interaction between the steady and unsteady ones. An analytical solution in the secondary wave has been obtained by Heaslet and Lomax in the linear case, and this linear solution has been borrowed to give an approximate solution by Bai and Wu for the nonlinear case. The structure of the secondary shock wave and the appearance of various force stages are two issues not yet considered in previous studies and has been studied in the present paper. A self-similar solution is obtained for the secondary shock wave, and the reason to have an initial force plateau as observed numerically is identified. Moreover, six theoretical characteristic time scales for pressure load variation are determined which explain the slope changes of the time-dependent force curve.     

Detection of aerosol pollution sources during sandstorms in Northwestern China using remote sensed and model simulated data

The present paper has used a comprehensive approach to study atmosphere pollution sources including the study of vertical distribution characteristics, the epicenters of occurrence and transport of atmospheric aerosol in North-West China under intensive dust storm registered in all cities of the region in April 2014. To achieve this goal, the remote sensing data using Moderate Resolution Imaging Spectroradiometer satellite (MODIS) as well as model-simulated data, were used, which facilitate tracking the sources, routes, and spatial extent of dust storms. The results of the study have shown strong territory pollution with aerosol during sandstorm. According to ground-based air quality monitoring stations data, concentrations of PM₁₀ and PM_2.5 exceeded 400?μg/m³ and 150?μg/m³, respectively, the ratio PM_2.5/PM₁₀ being within the range of 0.123–0.661. According to MODIS/Terra Collection 6 Level-2 aerosol products data and the Deep Blue algorithm data, the aerosol optical depth (AOD) at 550?nm in the pollution epicenter was within 0.75–1. The vertical distribution of aerosols indicates that the Cloud-Aerosol Lidar and Infrared Pathfinder Satellite Observations (CALIPSO) 532?nm total attenuates backscatter coefficient ranges from 0.01 to 0.0001?km^?1?×?sr^?1 with the distribution of the main types of aerosols in the troposphere of the region within 0–12.5?km, where the most severe aerosol contamination is observed in the lower troposphere (at 3–6?km). According to satellite sounding and model-simulated data, the sources of pollution are the deserted regions of Northern and Northwestern China.     

Kink mode m = 1 in magnetic tube with discontinuous magnetic field

In this paper, we study conditions of realization and stability of kink modes with azimuthal wave numbers $m=\pm 1$ in cylindrical plasma flex with twisted magnetic field and homogeneous current along its axis. We assume permanent axial magnetic field both inside and outside the flex, surrounded by currentless plasma. Azimuthal magnetic field decreases inversely proportional to the distance from the boundary beyond the flex. We derived dispersion equations for stable and unstable modes in approximation of “thin” plasma flex. The analysis of equations has been provided for the case of discontinuous axial magnetic field on flex’s boundary. Conditions of propagation of wave modes have been defined. It was shown, that unstable modes can be implemented in certain interval of longitudinal wavenumbers. Results can be applied for the interpretation of solar magnetic tubes behavior, using measurements, provided by spacecrafts.