An update global model of hmF2 from values estimated from ionosonde and COSMIC/FORMOSAT-3 radio occultation

In this paper, we present our recent work on developing an updated global model of the ionospheric F2 peak height hmF2 parameter by combining data from the Constellation Observing System for Meteorology, Ionosphere and Climate (COSMIC/FORMOSAT-3) radio occultation (RO) measurements and from the extended global ionosonde stations. In particular, 10 Chinese ionosonde stations’ data are newly introduced into this study. The modeling technique used is based on a two-layer empirical orthogonal function (EOF) expansion. Global distributions of hmF2 maps calculated using the newly constructed global model and the one provided by the International Reference Ionosphere model (IRI-ITU-R) are compared with the global distributions of hmF2 obtained by the COSMIC RO measurements and quantitative statistical analysis of the differences between the model results and those of the COSMIC RO measurements is made for the low (2008) and high (2012) solar activity years. The obtained average root-mean-square differences (RMSEs) for our model are 27.7 km (11.1%) and 31.0 km (9.8%), respectively for the years 2008 and 2012, whereas those for the IRI-ITU-R model are 39.9 km (16.9%) and 35.0 km (11.6%), respectively. Comparison of the results calculated both by our model and the IRI-ITU-R model with the digisonde observation is also made. The comparisons show that the newly constructed global hmF2 model can reproduce reasonably well the observations and perform better than IRI-ITU-R model.     

一种翼身融合飞行器的失速特性研究

翼身融合（BWB）布局飞行器作为下一代商用飞机的主要构型之一，越来越受到重视。对于翼身融合飞行器的研究主要针对其巡航状态的特性，而对其失速特性的研究较少。对一种翼身融合客机构型进行风洞试验研究，采用测力试验方法对其无增升装置的构型，以及具有翼梢小翼、前缘缝翼和机身上部双吊舱的组合部件构型下的纵向特性进行研究，特别是对其失速特性的分析，并通过二维粒子图像测试技术以及油流试验对其失速过程的流动机理进行研究。结果表明，无增升装置的基本构型下，翼身融合飞行器可以保持低速飞行，而各组合构型都具有提高最大升力系数的作用。对失速过程的分析表明，随着迎角的增大，飞机表面流场分离区域从翼梢开始逐渐向翼根以及机身发展，当外翼段完全处于分离区域时，飞机并不会马上失速，因为中心体同样具有提供升力的作用，且中心体的流动分离较外翼的流动分离更晚，所以当外翼在失速迎角出现升力损失时可以通过中心体的升力进行补偿，维持其低速飞行状态，真正的失速发生在中心体出现流动分离之后。     

Evaluation of global modeling of M(3000)F2 and hmF2 based on alternative empirical orthogonal function expansions

Global modeling of M(3000)F2 and hmF2 based on three alternative EOF (empirical orthogonal function) expansion methods is described briefly. Data used for the model construction is the monthly median hourly values of M(3000)F2 from the ionosonde/digisonde stations distributed around the world for the period of 1975–1985 and the hmF2 data of the same period converted from the measured M(3000)F2 based on the strong anti-correlation existing between them. Independent data of a low (1965) and a high (1970) solar activity year are used to validate the three alternative models based on different EOF expansion methods. Comparisons between the modeled results and observed data for both the low (1965) and high (1970) solar activity years showed good agreement for both M(3000)F2 and hmF2 parameters. Statistical analysis on the differences between model values and observed data showed that all the three alternative models (Model A, B and C) based on the different EOF expansion methods have better agreement with the observed data than the models currently used in IRI. All three alternative EOF based models have almost the same accuracy. Discussion on the preference of the three alternative EOF based models is given.     

小型化精密电机轴向预紧力调整研究

通过对液浮陀螺电机轴向预紧力调整情况及声音异常现象的分析,归纳和完善了电机轴向预紧力调整过程中的经验调法,并对电机轴向预紧力的量化调整进行了摸索和探讨,提出了较为可行的解决措施,从一定程度上保证了电机装调质量,提高了小型化精密电机装调合格率。     

Validation of B2bot in the NeQuick model during high solar activity at Hainan station

NeQuick ionospheric electron density model, which has been developed to version 2, produces the full electron density profile in the ionosphere. Each part of the profile is modeled using Epstein layer formalism. Simple empirical relations are used to compute the thicknesses of each layer. In order to validate the B2_bot parameter in the NeQuick model during high solar activity, we use the data at Hainan, China (109.1°E, 19.5°N; Geomagnetic coordinates: 178.95°E, 8.1°N), measured with DPS-4, and study the diurnal and seasonal variations of B2_bot, ΔB2 (B2_best − B2_NeQuick 2) and the seasonal median values of B2_best/B2_NeQuick 2 at that region. The results show that, (1) The differences between B2_best and B2_NeQuick 2 have diurnal and seasonal variations. (2) The diurnal variations of B2_NeQuick 2 are smaller than those of B2_best. (3) Generally, except for early morning the experimental values are properly reproduced. (4) Generally, during morning the NeQuick model has an underestimation. The magnitude of underestimation varies with LT and season.     

某型飞机连接螺栓断裂分析和排除

批量生产的飞机出现螺栓断裂，给飞行留下安全隐患。应深入分析其断裂原因，制定针对性排除方案，找出恰当、有效地防止此类现象发生的改进方法，以保障飞行安全。     

等臂杠杆式小力值标准装置关键技术研究

为了解决高准确度的小力值传感器和测力仪的校准问题,设计了一套小力值标准装置,其关键技术包括杠杆平衡系统的设计、专用砝码的设计、配平机构的设计等几个方面。这些关键技术保证了本标准装置的准确度,为小力值的计量校准提供了标准保障。     

MB26镁合金微弧氧化陶瓷膜层性能

文摘利用扫描电镜、表面性能测试仪和电化学测试技术等研究了在铝酸盐电解液中,不同电流密度和氧化时间对MB26镁合金微弧氧化膜的表面形貌、厚度、结合力以及耐蚀性等性能的影响。结果表明:随氧化时间和电流密度的增加,MB26镁合金微弧氧化膜层中的微孔数量减少,但孔变深。膜层厚度随氧化时间和电流密度的增加而线性增加,但与基体的结合力随之降低。氧化膜的耐蚀性随氧化时间和电流密度的增加呈先增加而后减小的趋势,该合金在铝酸盐体系中微弧氧化的最佳工艺为电流密度0.2 A/cm2,氧化时间40 m in。     

计算机生成兵力建模仿真支撑框架

计算机生成兵力CGF(Computer Generate Force)建模仿真支撑框架为仿真的快速开发提供支持.根据建模仿真领域的相关研究,提出组装是实现这一目标的有效途径.可组装性是对可重用能力的更高要求,需要必要的框架、知识主体、工具、技术和标准,以有效地实现仿真资源的集成、互操作以及重用.为了实现组装过程的自动化,支撑框架通过对典型CGF仿真开发过程进行分析,提出了相关关键技术,并给出了支撑框架的层次结构视图,为原型系统的构建提供了依据.支撑框架通过对模型规范的研究,实现了仿真概念模型的模板,使框架工具能以一致的方式对仿真模型进行表示和操作.      

基于视加速度的固体火箭发动机飞行比冲估算

建立了基于遥测视加速度的推力及比冲计算模型,模型中考虑了附加质量对发动机推力的影响,对固体火箭发动机飞行试验推力及比冲进行了计算,并与利用标准内弹道预示程序重新预示的发动机推力及比冲进行了对比,两种方法计算结果一致。算例表明,利用飞行试验遥测视加速度计算发动机推力及比冲的计算模型正确,有关参数的选取和处理方法可行;该方法可准确再现发动机飞行过程的实时推力和比冲;可有效用于发动机飞行试验结果的快速分析与评估。