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《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2020,65(7):1701-1713
Equatorial plasma bubbles (EPBs) are common features of the equatorial and low-latitude ionosphere and are known to cause radio wave scintillation which leads to the degradation of communication and navigation systems. Although these structures have been studied for decades, a full understanding of their evolution and dynamics remains important for space weather mitigation purposes. In this study, we present cases of EPBs occurrences around April and July 2012 geomagnetic storm periods over the African equatorial sector. The EPBs were observed from the Communications/Navigation Outage Forecasting System (C/NOFS) and generally correlated well to the ionospheric irregularities observed from the Global Positioning System total electron content (GPS-TEC) measurements (rate of TEC change, ROT). This study revealed that the evolution of the EPBs during moderate storms is controlled by the strength of the daytime equatorial electrojet (EEJ) currents regardless of the strength of the equatorial ionization anomaly (EIA), the latter is observed during the July storm case in particular. These effects were more evident during the main and part of the early recovery phases of the geomagnetic storm days considered. However, the evening hours TEC gradients between regions of the magnetic equator and ionization crests also played roles in the existence of ionospheric irregularities. 相似文献
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本文提出了一种基于虚拟页地址映射的NAND Flash管理算法.该算法通过定义坏块表、对应表等结构,以及设计的坏块替换策略和虚拟页地址到实际物理页地址的转换算法,实现上层软件采用虚拟地址对NAND Flash的无坏块连续页地址访问.该算法是一种高效的地址映射算法,能高效地对数据进行索引,占用SRAM空间较少,使系统达到高性能,并使得闪存使用的更加稳定持久. 相似文献
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《中国航空学报》2020,33(2):391-406
A thermal-solid-liquid complex operational environment induces structural interface developing a typical coupling sliding/impact wear behavior. It results in contact damage until systems fail, which may cause significant economic losses and catastrophic consequences. The key point of solving this problem is to reveal the coupling damage mechanism of the sliding/impact behavior in typical systems and life characterization under a complicate evolving environment. This has been a hot topic in the area of mechanical reliability. The main work in this paper can be concluded as follows. Firstly, the main industries in which the “sliding/impact behavior” takes place have been introduced. Then, existing studies on the wear mechanism and degree analysis are presented, which includes surface morphology analysis, wear debris analysis, and wear degree measurement. Meanwhile, existing problems in theoretical modeling and experiments in current research are summarized, so as to point out a bright direction for future research on wear prediction. They include interface contact modeling, mathematic coupling mechanism modeling, wear equation establishment, and wear life characterization, which can provide some new ideas for improving the existing studies on the sliding/impact wear behavior. 相似文献
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分析了 K8、 JL8机翼接头孔精加加后与检验量规位置协调的条件,介绍了为提高它们之间协调准确度所采取的措施及其效果。 相似文献
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进气道喘振诱发因素及其可靠性分析 总被引:1,自引:0,他引:1
针对飞机进气道的典型故障-喘振的诱发因素进行全方位的分析论证,并为从事航空工程的人员提供一种对动力装置整体性能进行可靠性评估方案,篇末对世界上比较先进的进气道气动设计思想及其喘振机理进行分析,可以为飞机设计师在设计飞机过程中具体分析问题提供一定的参考。 相似文献
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赵承龙 《南京航空航天大学学报》1990,(2)
本文在阐述基准的热力学概念基础上,提出了燃气基准的计算方法,应用CHAPPELL推荐的有关燃气热力性质表达式,导出计算燃气基准的公式,通过微机计算,将结果整理成燃气基准的有关表、图。 相似文献
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40Gh/8系统的应用面临光信号的色散、衰减、交换、编码等方面技术的挑战。利用固定补偿模块或源色散补偿技术可以实现光的精确色散及补偿。赖曼式放大器对40Gh/s系统的光传输提供了有力的技术支持,利用赖曼放大器以及全光交换机或光电光交换机则可以实现光信号的有效放大和高性能交换,而带外FEC技术和相应的编码技术可以进一步提高系统的容错能力及传输速率。 相似文献
10.
A numerical procedure for the calculation of the transonic dip of airfoils in the time domain is presented. A viscous-inviscid aerodynamic interaction method is taken to calculate the unsteady aerodynamic loads. In the present case the integral boundary layer equations are coupled with the Transonic Small Disturbance (TSD) Potential Equation. The coupling between structural motion and aerodynamic loads is carried out using State Space equation. It is solved by State Transition Matrix technique. Results are presented for NACA 64A010 and NLR 7301 airfoils with structural data from Isogai and DLR, respectively. Comparisons show good agreement with other numerical results. Certain deviations of experimental data taken from literature need more insight in the detailed test conditions. 相似文献