航天器基础激励SEA建模方法

针对航天器力学环境试验中随机横向基础激励高频预示技术开展了建模方法的研究。首先建立典型结构的有限元模型并开展仿真计算,获取背地板面内振动数据、连接环弯曲振动数据及振动台横向振动数据;进而分别建立背地板受纵向振动约束载荷、连接环受弯曲振动约束载荷的SEA模型,并将有限元计算结果作为激励源数据,利用统计能量分析（SEA）方法开展仿真分析,得到了航天器横向基础激励SEA建模的一般方法和步骤。研究表明:横向基础激励下,可将环境试验中获取的振动台数据以弯曲波的形式施加到连接环上,进行航天器高频响应SEA预示。     

气流激励下叶片振动响应分析方法

为开展气流激励下叶片振动响应分析方法研究,建立了气动激振力预估方法,采用非线性谐波法对叶排进行三维非定常流动分析,获得叶片表面的脉动压力,编制流固转换程序,计算叶片所受的气动激振力.建立了叶片气动阻尼分析方法,基于能量法和弱耦合分析法,对叶片与流场进行流固弱耦合分析,将气动力对运动的叶片所做的气动负功等效为黏滞阻尼力所...     

多绕组双流发电机励磁调压系统建模与Saber仿真

双流发电机励磁调压系统对发电机交直流电源的输出具有重要作用。文章主要分析了励磁调压系统的组成及工作原理,系统分别采用交/直流调压器(WZT-3型/SLT型),实现飞机发动机起动所需 115/200V、400Hz交流电和 28/56 V、0～70 V直流电的输出。采用 Saber建立仿真模型,仿真结果验证了励磁调压系统的可行性。     

Large eddy simulations of a turbulent mixing layer periodically excited with fundamental and third harmonic frequency

A better understanding of the mixing behavior of excited turbulent mixing layers is critical to a number of aerospace applications. Previous studies of excited turbulent mixing layers focused on single frequency excitation or the excitation with fundamental and its second harmonic frequency. There is a lack of detailed studies on applying low and higher frequency excitation. In this study, we have performed large-eddy simulations of periodically excited turbulent mixing layers. The excitation consists of a fundamental frequency and its third harmonic. We have used phase-averaging to identify the vortex structure and strength in the mixing layer, and we have studied the vortex dynamics. Two different vortex paring mechanisms are observed depending on the phase shift between the two excitation frequencies. The influence of these two mechanisms on the mixing of a passive scalar is also studied. It is found that exciting the mixing layer with these low and high frequencies has initially an adverse influence on the mixing process; however, it improves the mixing further downstream of the splitter plate with the excitation using a phase shift of $\mathrm{\Delta }\varphi =\mathrm{\pi }$ showing the best mixing performance. The present works shed lights on the fundamental vortex dynamics, and has great potential for aeronautical, automotive and combustion engineering applications.     

低功率霍尔推力器束流发散和推力矢量偏心特性研究

为了准确掌握不同工况下混合励磁模式低功率霍尔推力器束流发散和推力矢量偏心特性，凭借自主设计和改进的一套快速评估霍尔推力器束流发散角和推力矢量偏角原位集成诊断装置，系统研究了推力器在不同阳极质量流率、磁场、电场下束流分布和推力矢量偏心特性的变化规律。结果表明，束流发散角随阳极质量流率（0.65mg/s~0.95mg/s）和磁场强度（112Gs~142Gs）的变化呈现负相关的特性。当阳极质量流率0.95mg/s，束流发散角降到29.1°（＜30°）。推力矢量偏角随阳极质量流率和磁场强度的变化分别存在极大值（1.19°）和极小值（0.91°）。束流发散角、推力矢量偏角在250V~330V放电电压范围内基本保持不变。