局部弯矩对复合材料结构连接区的影响

本文选取部分不同连接形式的复合材料连接试验,首先按一般结构强度设计时将连接区视为理想化的模型预算结构破坏模式及最大承载值,再结合试验结果分析不同连接形式中影响破坏的关键原因,相互比较,寻求较合理的复合材料连接形式,避免复合材料结构连接设计中的不足。     

我心目中的空管人

空管,我并不陌生,甚至曾经走得很近。空管,也曾是我为之努力的理想。本科四年,在飞行学院学的正是空中交通管制,而且还是该校的第一届“。右转30度”“爬升至9000米报告”,面对模拟机上密密麻麻的飞机,一条条指令由我们口中发出,那是一种自豪,那更是一种责任。模拟机训练构建了     

EXPERIMENTAL INVESTIGATION ON R134A AIRBORNE VAPOR-COMPRESSION REFRIGERATION SYSTEM

The airborne high power electrical equipments have been widely used in modern aircrafts, which conse- quently causes the dramatic increase of heating load up to dozens of kilowatts. Accordingly, vapor-compression re- frigeration system （VCRS） with lower engine bleed air and larger refrigeration capacity has been paid much atten- tion in recent years. Therefore, based on the analysis of the characteristics of VCRS, an experiment system of VCRS using R134a is set up to simulate operation performances. The influences of different parameters including evaporation pressure, condensing pressure, refrigerant mass flow rate and compressor rotation speed are also in- vestigated. The impacts of different parameters on the system performance are various. This work can help to es- tablish the specific control law under different work conditions.     

漂亮的军火出口成绩单 2004年俄罗斯军火销售的绩效评析

在政府的积极推动下．俄罗斯2004年的军火销售再度取得55亿美元的亮丽成绩，销售的种类和层次不仅已有所提升，在北非和阿拉伯半岛的军火市场亦有所突破。不过俄国军火企业的基本问题倘无法获得解决，对其未来发展恐怕会有相当影响，非常值得注意。     

应用文教学与Web Quest模式

在传统的应用文教学中大多只是注重向学生讲授应用文的基本格式而忽略了教学方法的优化.应用文写作教学的整体优化原则要求按教学效果和时间耗费这两个准则来实施教学,研究应用文写作教学的组成要素以及这些要素之间的相互作用、相互联系,从而达到整体优化目标。论文通过分析应用文写作课程和Web Quest网络教学模式特点,结合教学经验探讨了Web Quest在应用文写作课程中的应用模式。     

"南北钦防"人力资源管理的思考

广西将启动"南北钦防北部湾城市群"协调发展规划,在北部湾地区形成大开发、大建设、大工业、大发展的格局。经济发展需要大量高素质的人才,建立"南北钦防"的人才高地是摆在我们面前非常重要而现实的问题,"南北钦防"的人力资源管理应该打破常规、不拘一格,不断健全激励制度、完善人才政策,为经济发展服务。     

AE9, AP9 and SPM: New Models for Specifying the Trapped Energetic Particle and Space Plasma Environment

The radiation belts and plasma in the Earth’s magnetosphere pose hazards to satellite systems which restrict design and orbit options with a resultant impact on mission performance and cost. For decades the standard space environment specification used for spacecraft design has been provided by the NASA AE8 and AP8 trapped radiation belt models. There are well-known limitations on their performance, however, and the need for a new trapped radiation and plasma model has been recognized by the engineering community for some time. To address this challenge a new set of models, denoted AE9/AP9/SPM, for energetic electrons, energetic protons and space plasma has been developed. The new models offer significant improvements including more detailed spatial resolution and the quantification of uncertainty due to both space weather and instrument errors. Fundamental to the model design, construction and operation are a number of new data sets and a novel statistical approach which captures first order temporal and spatial correlations allowing for the Monte-Carlo estimation of flux thresholds for user-specified percentile levels (e.g., 50th and 95th) over the course of the mission. An overview of the model architecture, data reduction methods, statistics algorithms, user application and initial validation is presented in this paper.     

Random signal radar - a winner in both the military and civilian operating environments

Besides some general requirements, modern military radars should possess excellent LPI (low probability of intercept) properties. And civilian radars should satisfy the rigorous requirement of EMC (electro-magnetic compatibility) performance. The special features of random signal radar are analyzed here based on the different requirements for military and civilian use. Results show that random signal radar has excellent LPI property and EMC performance simultaneously, which can satisfy both military and civilian requirements.     

双轨法D-InSAR形变测量的误差分析

以InSAR和双轨法D-InSAR基本原理为基础,推导出基线误差、卫星平台高程误差、相位测量误差、外部DEM误差以及大气延迟误差对双轨法D-InSAR形变测量影响的关系式,并对这些关系式进行分析,揭示了这些误差对双轨法D-InSAR形变测量影响的规律。     

Research on influence of typical microstructure characteristics of Ni base single crystal on creep rupture and deformation analysis of turbo blade

Considering the influence of typical microstructure characteristics on creep performance,a series of UM-F single crystal alloys which had similar element components but different microstructures were used to analyze the relationship between creep life and microstructure characteristics of Ni base single crystal.Three main factors were proposed:misfit,volume fraction of precipitate and maximum matrix channel width.The Microstate parameter Ymicro was established to estimate the deformation state of the materials.The linear relationship between the initial value of microstate parameter Y0 and creep life under a certain temperature/load was affirmed.By analyzing the high temperature region of turbo blade using the material parameters of DD 3,the creep deformation and the life prediction of the critical points of blade were obtained and the result closed to the test.