飞机虚拟仪表建模仿真关键技术研究

将介绍虚拟仪表设计软件的设计思路和功能作用。首先介绍了现有的虚拟仪表设计方法，分析其优缺点；之后介绍自主研发的虚拟仪表设计软件的特点，分析设计思路，分解介绍各模块的功能，给出仿真案例及最后的仿真效果。该虚拟仪表设计软件完全自主研发，具有易用性、可迅速建模、容易更改，模块化，通用性等特点。     

不同直径光滑圆管中黄原胶溶液流动减阻特性的实验研究

采用实验的方法,测试了黄原胶溶液在不同直径的光滑管道流动中的减阻特性和管径效应。其中变化参数为：（1）管道直径,共有3种管径,分别为5、10和20mm;（2）黄原胶溶液的浓度,变化范围为50~550ppm;（3）流速,用广义雷诺数（ReM）来表征,变化范围为0~50000。实验测量了不同参数下的管道压降Δp和体积流量Q,得到了黄原胶溶液浓度与减阻率的关系,以及ReM数对沿程阻力系数λ的影响,观测到黄原胶溶液减阻具有很明显的浓度效应,即随着溶液浓度的升高减阻率不断增大,直至达到最佳饱和减阻浓度,减阻率基本保持恒定。还观测到黄原胶溶液在不同管径中高低流速下表现出减阻类型的差异。     

基于通航飞机DA40维修演示系统的开发

提高通用航空器维修人员的业务水平,是通用航空事业快速发展的基本保障。为满足通用航空维修运行的需要,研发针对通用飞机的维修演示系统平台,可有效提高维修人员的学习效率,且具有广阔的社会效益和经济效益。系统基于DA40飞机维修手册和维修培训教学大纲开发,能较好地测试演示系统各项功能的完整性,具有广泛的示范意义。     

ENGINE SENSOR FAULT DIAGNOSIS USING MAIN AND DECENTRALIZED NEURAL NET WORKS

ＡｎａｌｙｔｉｃａｌｒｅｄｕｎｄａｎｃｙｔｅｃｈｎｉｑｕｅｓｓｕｃｈａｓｅｘｔｅｎｄｅｄＫａｌｍａｎｆｉｌｔｅｒ，ｃｏｍｐｏｎｅｎｔｓｔｒａｃｋｉｎｇｆｉｌｔｅｒａｎｄｓｏｏｎｃａｎｄｅｔｅｃｔ，ｉｓｏｌａｔｅａｎｄａｃｏｍｍｏｄａｔｅｆａｉｌｕｒ...     

基底完全粗糙时太沙基地基承载力系数的解析解

当前普遍采用的太沙基极限承载力公式中并未给出承载力系数Nγ的解析形式,而且Nc的表达方式在不同资料中不统一。针对以上情况,根据地基土的极限平衡原理,研究得出了条形基础底面完全粗糙条件下太沙基极限承载力系数Nγ′、Nc′的解析解。然后计算得出太沙基极限承载力系数的曲线以供查用。以上成果可为太沙基地基极限承载力公式的应用及研究工作提供参考。     

先进通用飞机航电系统概述

阐述了通用飞机航空电子系统的发展及其综合化的系统架构,介绍了Smart Deck系统和Top Deck系统这两款先进通飞航电系统的设计特点、系统架构以及两款先进系统的共性,最后对通用飞机航电系统的发展提出了一些展望。     

轻型通用飞机起飞总重估算方法研究

飞机的起飞总重是飞机的重要设计参数,概念设计阶段首先要做的重要工作之一就是确定飞机的起飞总重。以四人座低速活塞螺旋桨飞机为例,采用任务剖面法和商载航程法分别对起飞总重进行了估算,并对两种方法进行了修正,在此基础上,取两个计算结果的平均值作为最终的起飞总重估算值。通过与对比机型的比较,验证修正后的计算方法和结果是准确合理的,为通用飞机起飞总重的确定和选择提供了参考。     

中国电动飞机技术创新与实践观点

电动飞机极大地提高了飞机的环保性、舒适性、维修性和经济性，是航空工业未来的发展方向。电动飞机应具备高气动效率、高推进效率、高结构效率、高能量密度，以提高航时。"十三五"期间，中国已完成2机首飞，2机取证。"十四五"期间，电动飞机研发应该以高功率高效率电推进系统为研发重点，以混合电推进系列飞机为研发核心，以现有新能源型号全寿命保障体系研究为关键，以拓展新型电动飞行器研发和标准构建为目标。     

LARES successfully launched in orbit: Satellite and mission description

On February 13th 2012, the LARES satellite of the Italian Space Agency (ASI) was launched into orbit with the qualification flight of the new VEGA launcher of the European Space Agency (ESA). The payload was released very accurately in the nominal orbit. The name LARES means LAser RElativity Satellite and summarises the objective of the mission and some characteristics of the satellite. It is, in fact, a mission designed to test Einstein's General Relativity Theory (specifically ‘frame-dragging' and Lense-Thirring effect). The satellite is passive and covered with optical retroreflectors that send back laser pulses to the emitting ground station. This allows accurate positioning of the satellite, which is important for measuring the very small deviations from Galilei–Newton's laws. In 2008, ASI selected the prime industrial contractor for the LARES system with a heavy involvement of the universities in all phases of the programme, from the design to the construction and testing of the satellite and separation system. The data exploitation phase started immediately after the launch under a new contract between ASI and those universities. Tracking of the satellite is provided by the International Laser Ranging Service. Due to its particular design, LARES is the orbiting object with the highest known mean density in the solar system. In this paper, it is shown that this peculiarity makes it the best proof particle ever manufactured. Design aspects, mission objectives and preliminary data analysis will be also presented.     

Stabilization of an injected conducting layer for artificially enhancing drag on orbital debris

The evolution of a magnetized conducting medium suspended in magnetic and gravitational fields is examined. In this paper some effects of the influence of velocity fields on the linear stability properties of such layers are investigated. A fully compressible, three-dimensional analysis of the layer is described. The relevant equations are derived and then solved by the MagnetoHydroDynamic SPEctral Compressible Linear Stability (MHDSPECLS) algorithm, a Chebyshev collocation code. The code allows for the computation of magnetic and thermal effects. A complete stabilization of the system is found above a critical velocity of approximately 2500 m/s.