小振幅振荡圆柱域内部的定常整流旋涡流动

对充满静止不可压缩粘性流体的圆柱形，当柱壁沿垂直于柱轴方向作小振幅简谐振荡时的内部流动进行了实验研究，发现柱壁振荡在圆柱域内也诱导形成旋涡形态的定常整流流动。流动图谱随不同的振荡参数组合呈现四涡形态、双涡形态以及足印状双涡和蝶状四涡的过渡形态，并初步给出了不同整流图谱随数变化的演化规律。     

关于三维Navier－Stokes方程的粘性项计算

借助于张量分析和张量计算，在贴体曲线坐标系下本文讨论了不同求解变量导致了粘性项个数上的重大差异和不同大小的计算量，并提出了便于粘性计算的最佳形式。文中借助于有限体积离散技术，通过引进两个对称辅助矩阵［Ａ］和［Ｂ］，使粘性项的计算量大大减少，这对完成三维粘性流的数值计算具有重要的指导意义。借助于上述方法，本文完成了某型真实进气道两种工况的三维粘性Ｎａｖｉｅｒ－Ｓｔｏｋｅｓ方程计算（即Ｍ∞＝３．０，α＝０°和设计工况Ｍ∞＝２．６５，α＝０°），获得了满意的全场结果；对于Ｍ∞＝２．６５的设计工况，同实验数据作了比较，符合良好。由于本文的方法明显的减少了粘性项的计算量且节省了大量内存，以致于使三维流场的Ｎ－Ｓ求解能在普通微机上进行。     

喷管潜入段二维两相冷流实验

建立了喷管潜入段二维两相冷流实验设备,进行了相应的实验。实验清晰地显示了在潜入喷管进口背壁凹区旋涡的产生、稳定、消失,以及粒子的冲刷、粘贴、脱落、沉积等反复作用的复杂现象,它们与流动的雷诺数、粒子的含量和尺寸、潜入喷管进口处的形状和潜入深度、背壁型面等因素有关。     

Streamer Evaporation

Streamer evaporation is the consequence of heating in ideal MHD models because plasma is weakly contained by the magnetic field. Heating causes inflation, opening of field lines, and release of solar wind. It was discovered in simulations and, due to the absence of loss mechanisms, the ultimate end point is the complete evaporation of the streamer. Of course streamers do not behave in this way because of losses by thermal conduction and radiation. Heating is also expected to depend on ambient conditions. We use a global MHD model with thermal conduction to examine the effect of changing the heating scale height. We also extend an analytic model of streamers developed by Pneuman (1968) to show that steady streamers are unable to contain plasma for temperatures near the cusp greater than ∼ 2 × 10⁶ K. This revised version was published online in June 2006 with corrections to the Cover Date.     

On adaptive spatial-temporal processing for airborne surveillanceradar systems

Implementing the optimum spatial-temporal (angle-Doppler) processor involves two crucial issues: the selection of processing configurations, and the development of adaptive algorithms which can efficiently approach the performance potential of the selected configuration. Among the three available configurations, the joint-domain, the cascade space-time, and the cascade time-space, this work shows that, in contrast to a popular belief, the detection performance potentials of both cascade configurations can fall far below that of the joint-domain optimum. In addition, this work presents a new adaptive algorithm, called the Joint-Domain Localized Generalized Likelihood Ratio detection (JDL-GLR), which is data efficient i.e., with fast convergence to the joint-domain optimum, as well as computationally efficient, together with such desirable features as the embedded constant false-alarm rate (CFAR) and robustness in non-Gaussian interference     

Further results on adaptive filtering with embedded CFAR

Among the few known adaptive filtering algorithms which have an embedded (integrated) constant false alarm rate (CFAR) performance feature, the generalized likelihood ratio (GLR) test algorithm has been found to be robust in non-Gaussian clutter. This paper examines the detection performance of the GLR algorithm in nonhomogeneous/nonstationary clutter environments which lead to nonidentical distribution of secondary (training) data. For two common types of nonhomogeneity, i.e., the so-called “signal contamination” and “clutter edge”, the asymptotic detection performance is derived and compared with simulations. These asymptotic results are relatively simple to use and they predict the GLR performance in nonhomogeneous environments quite well. The GLR performance loss due to the nonhomogeneity is also evaluated. It is found that the “generalized angle” between the desired and contaminating signal plays an important role in the study of the effects of signal contamination. It is also found that the performance degradation due to the clutter edge depends largely on the width of the clutter spectrum and target-clutter Doppler separation     

导弹飞行安全区确定

对导弹飞行安全区进行了确切定义,分别对正常飞行弹安全区和故障飞行弹安全区进行了定量研究。在研究故障弹安全区时,从对导弹飞行安全产生的最终效果出发,对各种故障进行了科学分类,并建立了各类故障的故障方程,进而给出了导弹飞行安全区的计算模型和方法,这些模型和方法不仅符合故障飞行的物理背景,而且工程计算简单可靠。     

航空嵌入式系统2000年问题分析及检测方法

通过对航空系统嵌入式计算机的应用分析,根据航空系统嵌入式计算机应用领域和重要性的不同,将航空系统分为机载电子系统,遥测与导航系统,设备开发、测试和综合系统,以及生产加工系统四个层次。并针对每个层次绝对时间的使用特征,从系统参数共享到底层电路构型,提出了各自相应的 Ｙ２ Ｋ 问题检查方法,以及相应的检查内容和责任单位。     

螺旋弹簧应力松驰实验研究

对导弹弹体及发动机中常用的压缩螺旋弹簧进行应力松驰实验研究,得到了这种弹簧在常温下长期贮在职的应力松驰方程,为导弹武器系统的质量评判和延寿提供了可靠的实验依据。     

铝合金锻件重复淬火保温时间对组织性能的影响

分析了铝合金锻件重复淬火保温时间的长短及其组织性能的影响情况。根据大量的试验数据,证实了重复淬火保温时间及时效保温时间的长短对锻件性能的直接影响,并以此确定了合理的工艺参数。