解析计算在月球中继卫星Halo轨道设计中的应用

面向月球中继卫星工程轨道设计需求,研究解析计算方法在地月系L2点halo轨道设计中的应用问题。在讨论圆型限制性三体问题三阶解析近似计算方法的基础上,分析了解析计算与数值计算的差异,给出了解析近似计算在工程约束下的适用范围,进而提出了基于解析计算的轨道设计和特征筛选方法。分别采用解析初值和数值初值进行halo轨道外推,比对验证采用解析计算设计轨道的可行性。研究结果表明,解析计算方法适用于月球中继卫星轨道的初步设计、特征分析和构型筛选。     

人机环境系统中CFD的研究

 采用ＣＦＤ技术对人机环境系统中的一个典型问题——飞机空调座舱的舒适性进行了数值模拟,建立了相应的数值模拟方法,扩展了原有算法。数值模拟的成功,充分展示了ＣＦＤ技术在人机环境系统中的作用与可能带来的效益。     

导弹水下点火的流体动力研究

对轴对称导弹水下点火这一非线性瞬态流动提出以下数学模型及求解方法。水流场假设为理想不可压势流,用边界积分方程法求解;喷管中的燃气流动按准一维非定常无粘完全气体流动处理,用逆步有限差分格式的特征线法求解;喷入水中的燃气流采用简化的等压泡模型,用Euler-Lagrange方法模拟气泡的演化。按照时间步进方法实现了水、气流动和物体运动的数值耦合求解。数值实验结果反映出导弹水下点火时水气流动的一些重要特性。     

TC11钛合金的组织及塑性与其断裂韧性及裂纹扩展速率的关系

研究了TCll合金的组织及拉伸塑性(ψ)与断裂韧性(K_(IC)及裂纹扩展(da/dN)的关系。指明:K_(IC)及da/dN与ψ的关系取决于合金的组织类型。对片状组织及等轴组织进行了具体分析。     

连续激光加热推力器性能的简化解析计算模型

针对具有开放式吸收室的连续激光加热推力器,通过合理简化和分析,建立了一维流推力     

抛物形吸气式脉冲爆震激光推力器性能预示的解析模型

考虑激光束、推力器构型以及大气环境三方面因素,建立了抛物形吸气式脉冲爆震 激 光推力器性能预示的解析计算模型。其中,将推力室内的流场发展过程分为吸收波和冲击波 衰减两个阶段,应用Sedov点爆炸理论,以等效锥形约束空间,引入单一的修正因子以反 映流场的不均匀性。计算表明,其结果同现有实验数据吻合。〖JP〗     

Analytical expression for distant retrograde orbits around a small natural satellite

An analytical expression for distant retrograde orbits (DROs) is obtained in this study. Owing to the fact that a planar DRO is a closed orbit and can be expressed as an approximately elliptical orbit, respective geometries and periods of DROs are analytically calculated. A switching point, where various properties of planar DROs change abruptly with an increase in the orbital radius, is determined. The Mars–Deimos system is taken as a case study in this work. The proposed method can be applied to cases where the Hill’s approximation of the restricted three-body problem is valid. Numerical calculations are performed to validate the proposed method.     

XNJD－1工业风洞数据采集与处理系统

本文对ＸＮＪＤ－１工业风洞数据采集与处理系统作了综合介绍。该系统具有同时进行测力测压试验的能力，并提供压力联机校正、模拟量通道标准信号校正功能。整个系统的设计包括了许多先进的仪器概念如：电子扫描测压，模拟量信号调理等。系统具有采集速度快、稳定性好、软硬件功能齐全、实时数据处理、快速提供实验数据报告及图表、使用及维修方便等特点。     

Cutting tool temperature prediction method using analytical model for end milling

Dramatic tool temperature variation in end milling can cause excessive tool wear and shorten its life, especially in machining of difficult-to-machine materials. In this study, a new analyt-ical model-based method for the prediction of cutting tool temperature in end milling is presented. The cutting cycle is divided into temperature increase and decrease phases. For the temperature increase phase, a temperature prediction model considering real friction state between the chip and tool is proposed, and the heat flux and tool-chip contact length are then obtained through finite element simulation. In the temperature decrease phase, a temperature decrease model based on the one-dimension plate heat convection is proposed. A single wire thermocouple is employed to mea-sure the tool temperature in the conducted milling experiments. Both of the theoretical and experi-mental results are obtained with cutting conditions of the cutting speed ranging from 60 m/min to 100 m/min, feed per tooth from 0.12 mm/z to 0.20 mm/z, and the radial and axial depth of cut respec-tively being 4 mm and 0.5 mm. The comparison results show high agreement between the physical cutting experiments and the proposed cutting tool temperature prediction method.