前缘形状对钝三角翼边界层稳定性及转捩的影响

选择典型高速流动条件,基于线性稳定性理论研究了不同前缘几何特征对典型大后掠角平板钝三角翼外形高速边界层流动稳定性及转捩的影响.研究表明,椭前缘（截面为椭圆）形状的变化仅影响前缘附近的流场特征和边界层流动稳定性;前缘截面长短轴比（形状因子）变大,前缘形状变尖,则横流速度变大,扰动波增长率变大;对于横流模态和第1模态,不同频率扰动波的中性点流向位置随着前缘形状因子变大而后移;对于第2模态,不同频率扰动波中性点的位置基本不变.转捩由第1模态主导,前缘形状因子变大,转捩流向位置后移.      

超声空化及其声流结构实验研究*

超声空化及其声流效应在医学、化工和能源等领域得到广泛应用。本文采用高速摄像和粒子图像测速系统分别研究了超声场下的空化形态和声流场结构的时空演化规律。实验研究了50W,100W,200W和250W等四种不同输入功率对18kHz的超声变幅杆附近空化及其声流场的影响。研究结果表明：（1）在变幅杆下端面处观察到由大量空化气泡均匀分布组成的倒置锥形空泡结构,并且锥形空泡结构为稳态流动结构。（2）在超声变幅杆附近产生了两种不同的声流形式,第一种是变幅杆底端的射流型声流,第二种是变幅杆两侧的回旋流。此外,通过研究空泡与声流场中最大速度点之间的空间对应关系,发现声流是因为空泡流动带动而产生的。（3）空间位置和输入功率能显著影响射流型声流的流场结构,但是对回旋流的影响十分微弱。     

基于量子级联激光器照明的高对比度红外内窥成像

对单丝直径为20μm,12×9阵列方形面阵的Ge-As-Te-Se组分光纤束进行了测试,并开展红外成像研究。利用5~11μm连续可调谐红外量子级联激光器作为光源,对光纤束损耗进行检测,传输损耗平均为1 dB/cm。设计并加工了基于像方远心成像的紧凑型物镜,总长13.6 mm,直径6 mm,最终实现了2 mm×2 mm视场内100μm分辨率传像。分别在量子级联激光器和非相干黑体光源的照明下,进行了环境温度对成像对比度影响的研究,结果表明,在环境温度较高(>40℃)的条件下,基于量子级联激光器照明可实现高对比度内窥成像。本文对于深入开展红外生物效应研究具有指导意义和实用价值。     

耦合失稳模式与控制策略综合验证技术

为实现宽速域大空域飞行,面对称布局逐渐成为新型航天飞行器的典型特征,随之而来的还有横航向耦合问题,以及由此导致的失稳现象等.文章阐述了新型航天飞行器横航向耦合问题的成因和研究重要性,给出了针对耦合失稳模式和新型控制策略的综合验证方案,通过CFD-RBD仿真方法验证了荷兰滚失稳模式和副翼操纵耦合失稳模式的正确性,通过风洞虚拟飞行试验技术验证了新型控制策略的有效性,它可降低舵偏需求45%以上.      

A displacement-based reference frame formulation for steady-state thermo-elasto-plastic material processes

A reference frame formulation for steady state thermo-elasto-plastic processes is presented. The displacement and history dependent response fields appear as the primary variables in this mixed formulation. Unlike displacement based Lagrangian formulations, our formulation does not require a transient analysis to simulate a steady state process and yields results that are free of numerical oscillations and which require considerably less computational effort. And unlike velocity based Eulerian methods, our formulation does not require free surface corrections or streamline integration algorithms. A laser surface treatment process is simulated and our results are in agreement with those obtained from a computationally intensive transient Lagrangian analysis.     

Improved Adaptive Augmentation Control for a Flexible Launch Vehicle with Elastic Vibration

The continuous development of spacecraft with large flexible structures has resulted in an increase in the mass and aspect ratio of launch vehicles, while the wide application of lightweight materials in the aerospace field has increased the flexible modes of launch vehicles. In order to solve the problem of deviation from the nominal control or even destabilization of the system caused by uncertainties such as unknown or unmodelled dynamics, frequency perturbation of the flexible mode, changes in its own parameters, and external environmental disturbances during the flight of such large-scale flexible launch vehicles with simultaneous structural deformation, rigid-elastic coupling and multimodal vibrations, an improved adaptive augmentation control method based on model reference adaption, and spectral damping is proposed in this paper, including a basic PD controller, a reference model, and an adaptive gain adjustment based on spectral damping. The baseline PD controller was used for flight attitude control in the nominal state. In the non-nominal state, the spectral dampers in the adaptive gain adjustment law extracted and processed the high-frequency signal from the tracking error and control-command error between the reference model and the actual system to generate the adaptive gain. The adjustment gain was multiplied by the baseline controller gain to increase/decrease the overall gain of the system to improve the system’s performance and robust stability, so that the system had the ability to return to the nominal state when it was affected by various uncertainties and deviated from the nominal state, or even destabilized.     

高能球磨条件下TiO2相变的实验研究

 采用高能球磨法处理二氧化钛（TiO₂）与双氰胺粉末混合物,对不同球磨时间和球磨转速条件下TiO₂的相变进行了研究。利用X射线衍射仪对回收产物的相组成进行表征。结果表明,在700 r/min的高速球磨条件下,TiO₂发生了由锐钛矿相向金红石相和Srilankite高压相的转变,随着球磨时间的增加,Srilankite高压相和金红石相的含量逐步增加并逐渐趋于平衡;进一步提高球磨转速至1 000 r/min,锐钛矿相向Srilankite高压相的转变占主导,更易于形成Srilankite高压相,Srilankite高压相的质量分数可增加至47.8%。     

An object tracking method based on guided filter for night fusion image

Online object tracking is a challenging problem as it entails learning an effective model to account for appearance change caused by intrinsic and extrinsic factors. In this paper, we propose a novel online object tracking with guided image filter for accurate and robust night fusion image tracking. Firstly, frame difference is applied to produce the coarse target, which helps to generate observation models. Under the restriction of these models and local source image, guided filter generates sufficient and accurate foreground target. Then accurate boundaries of the target can be extracted from detection results. Finally timely updating for observation models help to avoid tracking shift. Both qualitative and quantitative evaluations on challenging image sequences demonstrate that the proposed tracking algorithm performs favorably against several state-of-art methods.     

流体回路在轨泄漏检测与定位技术研究

流体回路是长期在轨飞行器较常用的主动热控制技术,通过泵强迫流体工质在设定的管道中循环流动进行可调节传热。在轨运行期间,流体外回路可能会因空间碎片撞击等多种因素而发生泄漏故障,从而影响整个回路的热控平衡,最终影响整个航天器的运行安全。通过对外回路的工质压力和温度特性进行仿真分析,提出采用RBF神经网络对压力、温度关键点数据进行反演,获得泄漏孔径大小和泄漏位置,从而对管路泄漏进行实时监测。