Study of the Microphonics for Prospective Space-Based Neutron and Gamma-Ray Detectors and Methods for its Suppression

The results of testing a number of space-based detectors that contain PMTs or high-voltage electrodes for the noise from the microphonics that occurs in the signal path due to external mechanical action have been presented. A method for the vibration isolation of instruments aboard a spacecraft has been proposed to reduce their responsivity to vibrations.     

The Stressed State of a Stiffened Conical Shell with Thermal Protective Coating with Temperature-Dependent Properties

The equations of the mathematical model are solved in terms of special functions. The results for the design scheme of the aircraft forebody are obtained with a guaranteed accuracy by the stable method of functional normalization.     

SIMULATION OF BLEED AIR BEHAVIOR DURING AIRCRAFT IN FLIGHT BASED ON FLOWMASTER

Bleed air system is one of the most important components of air management system(AMS).It acts as transfer pipes responsible for air supply at high temperature and pressure.The thermal and flow performance of the bleed air system is a key issue for the design of AMS since the characteristics of air source have a great influence on the anti-ice system,the environmental control system and other downstream system in need of high temperature pressurized air.Based on the one-dimensional lumped parameter technology,a computer analysis model of bleed air system is developed in order to analyze the thermal and flow behaviors of the nodal points in the pipeline network.The simulation are performed with a given flight assignment using the analysis model,and the results verify that the system meets the design requirements.     

Development and verification of an innovative photomultiplier calibration system with a 10-fold increase in photometer resolution

In this study, we construct a photomultiplier calibration system. This calibration system can help scientists measuring and establishing the characteristic curve of the photon count versus light intensity. The system uses an innovative 10-fold optical attenuator to enable an optical power meter to calibrate photomultiplier tubes which have the resolution being much greater than that of the optical power meter. A simulation is firstly conducted to validate the feasibility of the system, and then the system construction, including optical design, circuit design, and software algorithm, is realized. The simulation generally agrees with measurement data of the constructed system, which are further used to establish the characteristic curve of the photon count versus light intensity.     

Computational analysis of strength,stability, and durability for gas turbine engine exhaust frame

A computational technique, developed for analysis of strength, stability and low-cycle durability of GTE exhaust frame complex structure under operational and emergency loads is described. The presented technique, based on the ANSYS and STAR-CD engineering analysis software, and self-design software can improve the accuracy and efficiency of calculations, and reduce efforts on finite element mesh development, performing calculations and processing of results.     

起始年龄与二语语言能力相关性研究

近年来,中国的外语学习出现了低龄化的趋势,各种双语早教班和幼儿园的出现似乎在提醒人们,外语学习越早越好。语言习得关键期假说也成为二语习得领域的研究重点之一,语言学者们在外语学习的起始年龄对外语学习效率的影响力方面无法达成共识。在对比分析关键期相关研究的基础上,通过实证研究试图证明不同年龄开始接触英语的学习者在语言能力方面并没有显示出明显的差异,关键期假说不适用于主要基于学校教学的外语教学。     

基于.NET的航空锻造知识管理系统框架的研究

通过对目前国内航空锻造企业的调研针对航空锻造企业知识管理的需求,对航空锻造知识进行分类总结,利用面向对象技术建立了航空锻造模型。在VS2008的软件平台上提出了一种基于.NET平台的航空锻造知识管理系统框架,并以某一航空锻造企业为例开发了航空锻造知识管理系统,具有知识信息结构化、知识管理流程化、知识检索快捷化等特点,并实现了和CAPP系统集成,实现了锻造知识资源的共享,初步实现了锻造工艺的智能设计。     

Technique for physical simulation of gasodynamic processes in the turbomachine flow passages

In this paper, a technique for the refined determination of turbine stage model parameters to investigate gasodynamic processes in the turbine flow passages without regard to uncontrolled heat exchange with environment is suggested.     

Guidance law implementation with performance recovery using an extended high-gain observer

Guidance law of a homing missile is implemented using an extended high gain observer without the model assumptions on target maneuvers. First, for a class of multi-input–multi-output nonlinear systems, extended high-gain observers are used for output feedback control with partial practical stabilization. Then the method is applied to the guidance law implementation of a homing missile with bearing only measurement. Simulation results show satisfactory performance.