Nonuniform Three-dimensional Configuration Distributed SAR Signal Reconstruction Clutter Suppression

This paper deals with the problem of clutter suppression in spaceborne distributed synthetic aperture radar (D-SAR) with nonuniform three-dimensional (3D) configuration geometry. In order to make a breakthrough of the configuration limitation of the traditional space time adaptive processing (STAP) based on uniform array and improve the inhomogeneous clutter suppression performance, this paper considers signal reconstruction technique using array interpolation to process the D-SAR signal. An array interpolation signal reconstruction method based on pitching-partition is derived then a signal reconstruction 3D-STAP clutter suppression method applied to nonuniform 3D configuration is proposed. In particular, the proposed method is compared with conventional methods and the performance analysis is carried out based on simulations. The improvement factor (IF) for clutter suppression is imported and reported as a benchmark on the clutter suppression effect.     

Preparation and Characterization of Fe3O4/T-ZnOw Composites

Fe3O4/T-ZnOw composites are fabricated by depositing a layer of Fe3O4 film on the surface of tetrapod-shaped ZnO whisker (T-ZnOw) by ferrite plating method. The morphology, structure and magnetic properties of the composites are characterized by scanning electron microscopy (SEM), X-ray diffractometer (XRD) and vibrating-sample magnetometer (VSM), respectively. The effects of temperature and pH value of ferrite plating on the Fe3O4/T-ZnOw composites and the magnetic properties of composites are studied. It is shown that the chemical environment with pH value at 7.5 is most favorable for the ferrite plating processes by analyzing the main peaks intensity of Fe3O4 in the XRD patterns and the average diameters of the Fe3O4 crystalline. The increase of the ferrite plating temperature with pH value around 7.5 benefits the whole encapsulation of T-ZnOw by the Fe3O4 magnetic films. The composites exhibit ferromagnetic properties and show much lower magnetization intensity than bulk samples at the same magnetic field intensity.     

孔排布方式对多斜孔壁火焰筒传热特性影响的数值研究

为了探寻高效的冷却技术,将多斜孔壁冷却结构应用于燃烧室火焰筒中,在实际工作条件下,对三种孔排布方式的火焰筒冷却特性进行了数值模拟.研究了斜排孔阵的周向偏移量H相对周向孔间距p的变化(模型A:H/p=0.2;模型B:H/p=0.4;模型C:H/p =0.5)对冷却特性的影响.计算结果表明,在燃烧室进口条件相同时,H/p的变化对总冷却用气量的影响很小,但对火焰筒的传热特性有明显影响,模型C的冷却效果优于模型A和B,并且火焰筒出口的温度分布不均匀系数ε较小.     

模糊综合评价模型的R语言实现

利用R语言可跨平台操作以及对矩阵运算高速的特点,对改进的模糊综合评价模型进行了实现,并给出了实现各流程的实例,验证了R语言实现模糊综合评价模型在不同操作系统下运行的可靠性及有效性。     

Role of the inter-pass cooling rate in recrystallization behaviors of Ni-based superalloy during interrupted hot compression

The microstructural evolution of a Ni-based superalloy under interrupted hot compressive deformation with different cooling rates in the inter-pass stage is investigated. It is found that metadynamic recrystallization(MDRX) in the inter-pass stage is more sensitive to the accumulated strain than the deformation temperature which is above the recrystallization temperature. The variations of both the grain distribution and the texture intensity caused by MDRX during the interpass stage result in variations of the yield stress(YS) and the work hardening(WH) rate in each stage. Results also show that the MDRX process in the inter-pass stage has a considerable influence on the final microstructure of three-pass compression. The final grain distribution is more uniform,and the compression texture gradually transforms into recrystallization texture with an increasing degree of MDRX. In order to predict the MDRX fraction in the inter-pass cooling stage, a modified kinetic equation is established, which can reasonably predict the MDRX behavior under multi-pass compression with different conditions in the inter-pass stage. Meanwhile, the influence of the interpass cooling stage on the mechanism of dynamic recrystallization(DRX) is studied. It is universally acknowledged that the discontinuous dynamic recrystallization(DDRX) process is the major deformation mechanism for the Ni-based superalloy. However, the continuous dynamic recrystallization(CDRX) process is promoted in the compression stage with a decrease of the cooling rate in each inter-pass stage.     

凝胶推进剂直圆管流动特性探讨

分析了非牛顿流体的类型,认为在液体火箭发动机中有应用前景的凝胶推进剂类型应是有屈服应力的牛顿流体或者幂律流体,关键在于胶凝剂。研究了直圆管中凝胶推进剂的流动特性,依据剪切速率可以将凝胶推进剂在直圆管中的流动分为三个区域。在第二流动区中,可以用幂律流体推导的流阻方程计算管路流阻;在第三流动区,可以近似用牛顿流体流阻方程计算流阻。     

液体火箭发动机燃烧室壁温与火焰温度分布红外感应测量技术

在实验室条件下,采用热电偶和红外测温仪同时对不锈钢和带辐射涂层的铌合金表面的温度及燃气温度进行测量,应用温度测量值来修正材料表面的黑度值及燃气的黑度值,利用黑度测量结果对某发动机试车时的温度场进行了测量,并与燃气的理论计算黑度值进行了对比。试验结果表明,这种方法对铌合金材料的壁温测量结果比较准确,而对不锈钢材料壁温测量结果准确度不是很理想。红外测温技术对燃气的温度测量结果与计算结果比较接近。     

创新投入会导致审计溢价吗?

选取2010年至2017年中国沪深两市A股上市公司作为研究样本,探讨企业创新投入是否会导致审计溢价,以及政治关联、高新技术企业认定在调节二者关系中的作用。研究发现,创新投入显著提高了审计费用;相对于不存在政治关联的企业而言,创新投入导致的审计溢价在存在政治关联的企业中显著弱化;高新技术企业认定削弱了审计师因创新投入而收取审计费用的风险应对行为。研究表明,在审计定价过程中,要将企业创新纳入考虑范围,为审计师进行专项审计时合理定价提供实证支持;对于增加创新投入而可能承担的审计溢价,上市公司要积极与审计师沟通协商,降低信息不对称程度,尽可能减少创新投入带来的负面影响。     

无人机飞行试验参数辨识研究

针对大型无人机飞行试验,探讨了无人机气动导数的参数辨识过程。根据无人机飞行试验数据特点及模态激励方式,分析并实践了相应的数据处理过程,修正了试飞数据;结合参数的相关性分析,建立了合适的气动模型,进行了气动导数辨识并验证了部分导数,辨识结果是真实可信的。所研究内容对验证和优化无人机空气动力和飞控设计进而合理地评价无人机的性能和品质具有重要意义。     

事故推演建模技术研究

 在总结现有事故模型、复杂系统特性分析的基础上,提出基于系统学的事故模型——事故推演模型,该模型强调从分析系统各组成部分的耦合关系及系统涌现特性的角度揭示事故是如何发生的。针对目前尚缺乏成熟的方法来支持基于系统学的事故分析的现状,建立了与事故模型匹配的事故推演建模方法,层次化面向对象的Petri网（HOOPN）,给出HOOPN的形式化描述,分析了HOOPN对事故推演建模的支持能力,介绍了基于HOOPN的事故推演建模程序。最后利用HOOPN建立民用航空器盘旋进近过程的事故推演模型,并对模型进行定性分析,验证该方法的适用性。