复合材料整体化加筋壁板高速冲击损伤数值模拟

 以复合材料结构抗弹性能分析与设计为目的,根据纤维的线弹性假设和基体的粘弹性假设,推导了复合材料单向板的粘弹性本构关系,导出了高应变率下复合材料层板的一阶剪切理论,建立了复合材料整体化加筋壁板高速冲击有限元分析模型.该模型引入界面单元模拟复合材料层间分层以及筋条与壁板间的脱粘损伤,结合Hashin失效准则进行筋条和单层板面内损伤识别,引入材料刚度退化,采用非线性有限元方法,研究了复合材料加筋结构高速冲击的破坏过程及损伤特性.数值分析结果与实验结果吻合良好,证明了该方法的合理有效性.探讨了筋条参数对高速冲击损伤的影响规律,获得了一些有价值的结论.     

障碍物对脉冲爆震发动机性能影响的数值模拟

运用计算流体力学方法计算了理想脉冲爆震发动机（PDE）单次爆震的性能参数,并和Wintenberger半分析模型进行了对比,研究了圆环形障碍物阻塞比和节距内径比对空气流动损失和脉冲爆震发动机单次爆震性能的影响,并与连续的多脉冲爆震实验的相关结果做了比较。研究结果表明,数值模拟计算得到的冲量和Wintenberger半分析模型得到的冲量非常接近,佐证了数值模拟方法和结果的正确性;障碍物阻塞比增大、节距内径比减小或进口速度增大,空气流过障碍物时的总压恢复系数减小,流动损失增大;障碍物阻塞比增大,单次爆震的体积比冲减小,单位燃油消耗率增大,性能降低;当阻塞比为41％时,体积比冲为理想爆震管体积比冲的92％,损失了8％;障碍物节距内径比增大,单次爆震的体积比冲先减小后增大,而单位燃油消耗率先增大后减小,不同节距内径比的体积比冲为理想爆震管体积比冲的94％左右,不同节距内径比对性能影响规律与多次脉冲爆震实验结果趋势符合。     

旋转平板型叶端气膜冷却实验研究

在相似理论指导下, 对旋转系流动与换热方程以及边界条件进行无量纲化, 得出了描述旋转气膜冷却效率与换热系数的一系列准则, 设计并建立了实验台, 解决了从高速旋转部件上引出测试信号而不失真及对旋转试件进行强电加热等问题, 并在旋转情况下, 对常用的平板型叶端气膜冷却效率及其换热系数进行了实验研究, 并总结出可供工程参考的准则公式.      

数学规划的物理模型及算法

利用力学原理，建立了用微分方程描述的带不等式约束优化问题的物理模型，用人工释能和摄动的思想，推广了现行的一些可行方向算法，并对算法的收敛性进行了讨论。     

Using GPS-SCINDA observations to study the correlation between scintillation,total electron content enhancement and depletions over the Kenyan region

This paper presents the first results of total electron content (TEC) depletions and enhancement associated with ionospheric irregularities in the low latitude region over Kenya. At the low latitude ionosphere the diurnal behavior of scintillation is driven by the formation of large scale equatorial depletions which are formed by post-sunset plasma instabilities via the Rayleigh–Taylor instability near the magnetic equator. Data from the GPS scintillation receiver (GPS-SCINDA) located at the University of Nairobi (36.8°E, 1.27°S) for March 2011 was used in this study. The TEC depletions have been detected from satellite passes along the line of sight of the signal and the detected depletions have good correspondence with the occurrence of scintillation patches. TEC enhancement has been observed and is not correlated with increases in S₄ index and consecutive enhancements and depletions in TEC have also been observed which results into scintillation patches related to TEC depletions. The TEC depletions have been interpreted as plasma irregularities and inhomogeneities in the F region caused by plasma instabilities, while TEC enhancement have been interpreted as the manifestation of plasma density enhancements mainly associated with the equatorial ionization anomaly crest over this region. Occurrence of scintillation does happen at and around the ionization anomaly crest over Kenyan region. The presence of high ambient electron densities and large electron density gradients associated with small scale irregularities in the ionization anomaly regions have been linked to the occurrence of scintillation.     

Variability of foF2 in the African equatorial ionosphere

This paper presents the impact of diurnal, seasonal and solar activity effects on the variability of ionospheric foF2 in the African equatorial latitude. Three African ionospheric stations; Dakar (14.8°N, 17.4°W, dip: 11.4°N), Ouagadougou (12.4°N, 1.5°W, dip: 2.8°N) and Djibouti (11.5°N, 42.8°E, dip: 7.2°N) were considered for the investigation. The overall aim is to provide African inputs that will be of assistance at improving existing forecasting models. The diurnal analysis revealed that the ionospheric critical frequency (foF2) is more susceptible to variability during the night-time than the day-time, with two peaks in the range; 18–38% during post-sunset hours and 35–55% during post-midnight hours. The seasonal and solar activity analyses showed a post-sunset September Equinox maximum and June Solstice maximum of foF2 variability in all the stations for all seasons. At all the stations, foF2 variability was high for low solar activity year. Overall, we concluded that equatorial foF2 variability increases with decreasing solar activity during night-time.     

Comparative evaluation of five global gravity models over a part of the Bay of Bengal

Several global gravity models (GGMs) are freely available in the public domain, which can be utilised to study the earth's gravity field in almost every part of the globe. The present study compared the free-air gravity anomalies calculated from the five GGMs EGM2008, EIGEN6C4, GECO, XGM2019e_2159, and SGG-UGM-2 archived by the International Centre for Global Earth Models (ICGEM) with respect to shipborne gravity in the Bay of Bengal. The average correlation coefficient and covariance are ～ 96 % and ～ 450mGal². The mean difference between the shipborne and the modelled gravity is ? 5 mGal. Relatively higher amplitude gravity differences observed at the continental-oceanic transition, the 85°E and Ninetyeast ridges, and the western basin are possibly due to high gradient, dominant density contrasts, and rugged topography. The average standard deviation and root-mean-square-error (RMSE) of the differences are ～ 6.5 mGal and ～ 7.5 mGal. A significantly lower standard deviation and RMSE found for the models generated at higher degree/order compared to lower degree/order is due to diminishing omission error of the GGMs with increasing degrees of truncation. The spectral analysis and coherence estimation of the modelled gravity demonstrate excellent correspondence for anomalies wider than ～ 25 km. The agreement between anomaly amplitudes and shapes and calculated statistics indicates that the accuracy and resolution of the modelled gravity data are certainly good enough for regional-scale studies aiming to map Moho topography and mantle structures. However, the delineation of shorter wavelength features originating from the shallow-level basement/sedimentary might be uncertain and requires further validations. The present study confirms that all five models show promising results in terms of their accuracy and resolution. Moreover, the SGG-UGM-2 and XGM2019e_2159 models compare favourably with respect to the GECO, EIGEN6C4 and EGM2008 models in the Bay of Bengal.     

一种基于滑动库的多模自适应控制方法

针对系统参数跳变时常规自适应控制闭环系统暂态响应差的问题,论文提出了一种基于滑动库的多模自适应控制方法。该控制器由多个参数已知的固定模型,一个自适应模型和一个滑动模型库构成。固定模型由被控对象在特定环境下的特征模型直接映射获得,其参数和其邻域一起覆盖被控对象的参数集;自适应模型对被控对象进行在线参数辨识,其参数被用来动态更新固定模型库;滑动模型库根据当前的工作点从固定模型库中选择离工作点较近的部分模型参与控制,优化控制模型集,减少计算量。仿真实验的结果表明了该方法的有效性。     

A NEW FATIGUE CUMULATIVE DAMAGE DYNAMIC INTERFERENCE MODEL

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