纵向加速流场中风速管系数的理论修正

基于理想不可压轴对称位流理论，求得一任意椭球在纵向加速流场中绕流的精确解。并以一根细长的棉球近似模拟风速管，求得均匀流中风速管系数理论值，以及在纵向加速流中它的相对偏差值。以两个长细比各为32和250的椭球为算例，得知在一般风洞实验段内存在的速度梯度下，风速管系数的相对偏差量很小。文中表1、表2所列不同加速下风速管系数的相对偏差值，可近似用来修正实际风速管，或根据流场加速程度选择合适的风速管外径的大小。     

三维接触问题的接触状态有限元解法及应用

在文献［１］的基础上论述了有摩擦、有间隙的三维弹性接触问题接触状态有限元解法，并通过理论考题进行了验证。最后，在应用部分对汽轮机汽缸法兰连接汽密性进行了计算。     

角速度波动检测技术研究

标准转台等旋转体在转动时产生的角速度波动对被标定设备的数据可信度有很大影响。本文主要论述了角速度波动检测的重要性和可能性，并对检测的方法进行了介绍，用时域等信号处理方法对角速度波动数据进行了分析。     

A novel method for importance measure analysis in the presence of epistemic and aleatory uncertainties

For structural systems with both epistemic and aleatory uncertainties, research on quantifying the contribution of the epistemic and aleatory uncertainties to the failure probability of the systems is conducted. Based on the method of separating epistemic and aleatory uncertainties in a variable, the core idea of the research is firstly to establish a novel deterministic transition model for auxiliary variables, distribution parameters, random variables, failure probability, then to propose the improved importance sampling(IS) to solve the transition model. Furthermore,the distribution parameters and auxiliary variables are sampled simultaneously and independently;therefore, the inefficient sampling procedure with an ‘‘inner-loop' for epistemic uncertainty and an‘‘outer-loop' for aleatory uncertainty in traditional methods is avoided. Since the proposed method combines the fast convergence of the proper estimates and searches failure samples in the interesting regions with high efficiency, the proposed method is more efficient than traditional methods for the variance-based failure probability sensitivity measures in the presence of epistemic and aleatory uncertainties. Two numerical examples and one engineering example are introduced for demonstrating the efficiency and precision of the proposed method for structural systems with both epistemic and aleatory uncertainties.     

空间站微重力环境研究与分析

太空中的微重力环境对基础科学研究和新技术开发具有重要意义,为了满足未来我国空间站开展微重力科学实验的需求,需要对空间站上的微重力水平进行分析和评估,指导高微重力要求实验载荷的布局和微重力实验期间的飞行任务规划。空间站上的微重力水平用加速度值度量,通常可以分为准稳态加速度、瞬态加速度和振动加速度。针对此问题调研总结了国际空间站的微重力研究情况,并以400 km轨道高度上100吨级"T"字型积木式空间站作为算例,估算其准稳态加速度大小及分布,并初步分析瞬态加速度水平的量级。结果表明,空间站准稳态加速度水平在1μgn量级,主要贡献来自重力梯度效应;瞬态加速度可达103μgn量级。文章对将来我国空间站微重力应用支持的设计工作有一定的借鉴意义。     

Formability enhancement in hot spinning of titanium alloy thin-walled tube via prediction and control of ductile fracture

The damage and fracture in hot spinning of titanium alloy is a very complex process under the combined effects of microstructure evolution and stress state. In this study, their dependences on processing parameters were investigated by an integrated FE model considering microstructure and damage evolution, and revealing the effects of microstructure and stress states on damage evolution. The results show that the inner surface of workpiece with the largest voids volume fraction is the place with...     

民用飞机融合式翼梢小翼优化设计

民用飞机性能的提高将在很大程度上依赖于降低空气阻力。在巡航状态下,如果能减小机翼的诱导阻力,则全机的减阻效果将会得到很明显的提高。因此,本文以民用飞机机翼为设计平台,通过加装融合式翼梢小翼来减阻,并在设计了初始小翼的基础上,将减阻作为设计目标,对翼梢小翼的平面几何形状进行优化,并对结果进行了流动机理分析。     

空中运动目标的识别和跟踪控制

针对空中运动目标的识别和跟踪,提出图像匹配算法和连通域算法相结合的方法。该方法主要用图像匹配算法获得目标的位置信息,当图像匹配算法失效时,则采用连通域算法重新捕获目标、获得图像模板。同时,为提高跟踪的实时性,采用最小二乘线性预测法来预测目标的运动轨迹。在实验室的目标跟踪系统平台上,该方法能够对运动目标进行稳定的识别和跟踪。     

Optimization of structural parameters for elliptical cross-section spiral equal-channel extrusion dies based on grey theory

The elliptical cross-section spiral equal-channel extrusion (ECSEE) process is simulated by using Deform-3D finite element software. The ratio m of major-axis to minor-axis length for ellipse-cross-section, the torsion angle u, the round-ellipse cross-section transitional channel L1, the elliptical rotation cross-section transitional channel L2 and the ellipse-round cross-section transitional channel L3 are destined for the extrusion process parameters. The average effective strain eave on cross-section of blank, the deformation uniformity coefficient a and the value of maximum damage dmax are chosen to be the optimize indexes, and the virtual orthogonal experiment of L16 (45) is designed. The correlation degree of the process factors affecting eave, a and dmax is analyzed by the numerical simulation results using the weights and grey association model. The process parameters are optimized by introducing the grey situation decision theory and the ECSEE optimal combination of process parameters is obtained: u of 120 , m of 1.55, L1 of 7 mm, L2 of 10 mm, and L3 of 10 mm. Simulation and experimental results show that the material can be refined with the optimized structural parameters of die. Therefore, the optimization results are satisfactory.     

跨声速风扇叶片反扭影响因素研究

基于结构几何非线性大变形的静态分析和流场分析,使用叶片反扭设计的流固双向耦合的数值模拟方法,得到NASA Rotor67跨声速风扇叶片的冷态加工叶型。研究了材料、气动工况、转速对叶片静态变形和反扭设计参数的影响。结果表明:转速对叶片反扭的影响最显著,气动工况次之,材料的影响最弱;另外,这三种因素和叶片反扭的关系,与其和叶片静变形量的关系有较大相关性。