基于单纯形加速法的消除重建坐标轴误差

将一个坐标系平移、旋转到第二个坐标系位置,以建立坐标系的三个点九个坐标为自变量,应用单纯形加速法优化,通过调整步长,最大程度地消除建轴误差。     

三通管复合胀形过程模拟

建立了三通管复合胀形的三维弹塑性有限元模型,研究了三通管液压复合胀形中,反压大小、加载路径以及加载时间等对胀形成形的影响。     

飞行器多学科设计优化中的灵敏度分析方法研究

近年来,在飞行器设计领域,多学科设计优化(MDO)方法得到了高度重视。灵敏度分析技术作为MDO的关键技术之一,被认为是处理飞行器MDO研究中四个复杂性问题的有力工具。本文对适用于飞行器MDO的灵敏度分析方法进行了系统研究。首先介绍了多种学科灵敏度分析方法,阐述了各种方法的原理,比较了各种方法的优缺点。在此基础上,进一步探讨了几种常用的系统灵敏度分析方法。最后,总结了各种灵敏度分析方法在飞行器MDO中应用的原则,并对发展适用性更广的广义灵敏度分析方法提出了建议。     

快速构建基于EZ-USB芯片的数据传输管道

通过深入剖析设备数据传输所面临的诸多问题及特点,给出一系列快速构造USB传输管道应遵循的原则,为设备接入主机提供一个简单、经济且可靠的传输方案。其核心是用标准USB总线接口、连接器及USBHUB实现传输的经济可靠;由功能强大的EZ-USB芯片和工具包简化接口电路及代码设计。     

飞行控制系统的快速原型设计

飞行控制系统设计是一个涉及控制、机械、电子和计算机等多个分系统的复杂系统工程,需要进行多学科、多专业的协同设计,虚拟样机技术从建模和仿真分析等多个方面为协同设计提供了技术和方法上的支持,而快速原型设计是基于虚拟样机的,快速生成物理样机的一种技术,可以看作是我国现阶段虚拟样机技术应用的一个廉价快速的替代方案。介绍了快速原型设计的概念,针对飞行控制系统的快速原型设计,讨论了与其有关的设计仿真软件、关键技术和实施方法。     

Influence of TiB2 particles on machinability and machining parameter optimization of TiB2/Al MMCs

In situ formed TiB₂ particle reinforced aluminum matrix composites (TiB₂/Al MMCs) have some extraordinary properties which make them be a promising material for high performance aero-engine blade. Due to the influence of TiB₂ particles, the machinability is still a problem which restricts the application of TiB₂/Al MMCs. In order to meet the industrial requirements, the influence of TiB₂ particles on the machinability of TiB₂/Al MMCs was investigated experimentally. Moreover, the optimal machining conditions for this kind of MMCs were investigated in this study. The major conclusions are: (1) the machining force of TiB₂/Al MMCs is bigger than that of non-reinforced alloy and mainly controlled by feed rate; (2) the residual stress of TiB₂/Al MMCs is compressive while that of non-reinforced alloy is nearly neutral; (3) the surface roughness of TiB₂/Al MMCs is smaller than that of non-reinforced alloy under the same cutting speed, but reverse result was observed when the feed rate increased; (4) a multi-objective optimization model for surface roughness and material removal rate (MRR) was established, and a set of optimal parameter combinations of the machining was obtained. The results show a great difference from SiC particle reinforced MMCs and provide a useful guide for a better control of machining process of this material.     

简析俄罗斯文化的双重性

俄罗斯民族是一个伟大的民族。地理位置与历史的造就使她具有了东西方文化的双重性及感性化的民族个性。这种文化特点对其民族产生了深远的影响。     

DLR-F4翼身组合体的阻力计算

为了考察自行研发的CFD软件的计算能力和阻力计算精度，本文采用LU—SGS方法、MUSCL差分格式和Baldwin—Lomax代数湍流模型，数值模拟了AIAA阻力计算工作室提供的DLR—F4翼身组合体的绕流流场，综合分析了easel和case2的气动力的计算结果，并与NASA Christopher L．Rumsey采用CFL3D6．0和AFRL/VAAC Don W．Kinsey采用Cobalt60提供的两组计算结果以及AGARD提供的两种不同风洞的测力试验结果作了比较。计算结果表明，本文计算精度与国外CFD软件相当。为了提高激波，边界层干扰的模拟精度，今后要重点加强湍流模型的应用研究。     

Global aerodynamic design optimization based on data dimensionality reduction

In aerodynamic optimization, global optimization methods such as genetic algorithms are preferred in many cases because of their advantage on reaching global optimum. However, for complex problems in which large number of design variables are needed, the computational cost becomes prohibitive, and thus original global optimization strategies are required. To address this need, data dimensionality reduction method is combined with global optimization methods, thus forming a new global optimization system, aiming to improve the efficiency of conventional global optimization. The new optimization system involves applying Proper Orthogonal Decomposition (POD) in dimensionality reduction of design space while maintaining the generality of original design space. Besides, an acceleration approach for samples calculation in surrogate modeling is applied to reduce the computational time while providing sufficient accuracy. The optimizations of a transonic airfoil RAE2822 and the transonic wing ONERA M6 are performed to demonstrate the effectiveness of the proposed new optimization system. In both cases, we manage to reduce the number of design variables from 20 to 10 and from 42 to 20 respectively. The new design optimization system converges faster and it takes 1/3 of the total time of traditional optimization to converge to a better design, thus significantly reducing the overall optimization time and improving the efficiency of conventional global design optimization method.     

卫星业务测控站在轨测试系统软件研究

探讨了卫星在轨测试系统软件开发平台以及测试软件的功能和实现。