离散光谱分辨率对喷流红外特性FVM计算的影响

建立了辐射传递方程(RTE)的有限元体积法(FVM)计算模型,研究了离散光谱分辨率对FVM计算精度的影响,提出了离散光谱分辨率无关解的概念,并编制了相应的FORTRAN源程序,结合大气飞行发动机标准算例进行了一系列计算和比较.结果表明;在给定的红外光谱域中,随着离散光谱的分辨率的提高,计算出的方向光谱辐射强度渐渐趋向于同一个值.在航空发动机喷流2～5μm红外光谱区间中,当划分150个以上等间隔光谱微元后,FVM可以保证达到离散光谱分辨率无关解.      

直升机附件舱温度场的数值模拟

为考查某型直升机附件舱的热控制能力,采用有限元软件分析了其在强制冷却和自然冷却情况下的温度场分布.应用非结构化网格和有限体积法进行计算区域和控制方程的离散,采用标准k-ε模型封闭湍流控制方程.针对3种冷却系统设计方案,分析了不同冷却气流进口尺寸、相对位置以及不同附件散热量对附件舱温度分布的影响,计算了自然冷却情况下附件舱密闭时的温度场.计算和试验结果均表明,所采用的冷却方案可以满足附件舱冷却的需要.      

大涡模拟模型环形燃烧室污染特性

在任意曲线坐标系下,采用大涡模拟模型环形燃烧室两相燃烧流场中污染物的生成.用亚网格涡破碎(EBU)燃烧模型估算化学反应速率;分别用NO亚网格动力学模型与CO亚网格模型来模拟NO和CO的生成;采用随机离散模型模拟气液两相湍流流动,两相之间耦合采用PSIC算法.计算结果与瞬态速度场、出口温度和污染物质量分数分布的实验数据比较吻合,表明大涡模拟方法和亚网格模型可以用来预估实际燃烧室两相喷雾燃烧流场和污染物生成过程.      

1553B总线接口SoC验证平台的实现

随着半导体技术的发展,验证已经成为SoC设计的瓶颈.分析了SoC验证面临的困难,结合1553B总线接口SoC芯片的具体实践,重点研究了SoC验证平台的一种构建实现方法.该方法提高了验证效率,缩短了整个设计验证周期.     

小推力航天器的地月低能转移轨道

 在限制性四体模型下研究基于小推力方式的地月低能转移问题,通过借助于平动点轨道的相空间结构来揭示小推力转移的机理。重点研究了小推力转移自由飞行段的构造：经由LL₁点穿越获得最小能量的低能转移;而经由LL₁点Halo轨道穿越,得到(M,N)圈穿越轨道;由于Halo轨道相对于平动点增加了一维度的选择,根据(2,2)圈穿越轨道构造该转移的自由飞行段。在地球势阱逃逸和月球势阱捕获段,分别设计了合适的小推力的控制律及发动机开/关机时间,成功实施近地球段的小推力加速和近月球段的减速。尽管未对所得到的结果进行优化,所得转移轨道的燃料消耗也与类似边界条件的SMART-1轨道基本一致。     

Aviation-oriented Micromachining Technology-Micro-ECM in Pure Water

This article proposes a precise and ecofriendly micromachining technology for aerospace application called electrochemical machining in pure water （PW-ECM）. On the basis of the principles of water dissociation, a series of test setups and tests are devised and performed under different conditions. These tests explain the need for technological conditions realizing PW-ECM, and further explore the technological principles. The results from the tests demonstrate a successful removal of electrolytic slime by means of ultrasonic vibration of the workpiece. To ensure the stability and reliability of PW-ECM process, a new combined machining method of PW-ECM assisted with ultrasonic vibration （PW-ECM/USV） is devised. Trilateral and square cavities and holes as well as a group of English alphabets are worked out on a stainless steel plate. It is confirmed that PW-ECM will be probably an efficient new aviation precision machining method.     

一种高效的基于可靠性的多学科设计优化方法(英文)

Design for modem engineering system is becoming multidisciplinary and incorporates practical uncertainties; therefore, it is necessary to synthesize reliability analysis and the multidisciplinary design optimization （MDO） techniques for the design of complex engineering system. An advanced first order second moment method-based concurrent subspace optimization approach is proposed based on the comparison and analysis of the existing multidisciplinary optimization techniques and the reliability analysis methods. It is seen through a canard configuration optimization for a three-surface transport that the proposed method is computationally efficient and practical with the least modification to the current deterministic optimization process.     

Imaging of target with complicated motion using ISAR system based on IPHAF-TVA

The technique of imaging a target with a complicated motion using an Inverse Synthetic Aperture Radar (ISAR) system is an effective tool in the field of radar signal processing. After the translational compensation, the received signal reflected from the target can take the form of a multi-component Polynomial Phase Signal (m-PPS), and the high quality ISAR image can be provided via the combination between the estimated parameters of the m-PPS and the Range Instantaneous-Doppler technique (RID). For a target with a high maneuvrability, the occurrence of scatterers Migration Through Resolution Cell (MTRC), caused by the rotational movement could be appearing. That is why the variation in the amplitude of the echo during the time of observation cannot be neglected. The purpose of this study is the parameters estimation of the m-PPS signal with order three in the case of the Time Varying Amplitude (TVA). The Improved-version of the Product High-order Ambiguity Function (IPHAF) with TVA is proposed to improve the quality of the ISAR image compared with traditional techniques based on a constant amplitude; the experimental outcomes confirm that the new IPHAF-TVA method presented in this study is an effective technique to make the ISAR image very clear.     

推进剂贮箱金属焊接件疲劳裂纹对应力强度因子影响的数值分析

卫星推进剂贮箱的焊接质量直接影响卫星的寿命和可靠性。文章通过仿真分析研究焊接残余应力对贮箱上已存在裂纹的影响。首先针对球壳模型和平板模型分别计算焊接残余应力,然后在应力强度值最大的危险区域引入裂纹,对不同角度和尺寸系数的裂纹对应力强度因子影响的数值和变化趋势进行分析。研究表明：起主要作用的是应力强度因子KI;KII受角度影响相对较大;KI和KII的最小值都在裂纹中心处;KIII基本随归一化裂纹前沿数值增加而增加。     

基于超声导波的返回舱热防护结构烧蚀层厚度监测方法

为实时监测航天器返回舱烧蚀层厚度,文章基于超声导波在双层板结构中的传播特性研究发现导波波速与烧蚀层厚度相关,故提出依据导波波速变化对结构烧蚀层厚度损失进行表征的方法,以及根据导波频散曲线和厚度敏感曲线选择适当的监测模态和频率的方法,可以实现烧蚀层厚度的高效率、高精度实时在线监测。有限元仿真和实验结果均验证了该烧蚀层厚度监测方法的有效性。