铜川新区采暖期PM_(2.5)浓度与气象条件关系探究

利用铜川市新区2013年11月至2014年3月PM2.5逐时浓度和距离最近的耀县气象观测站同步气象观测资料,分析了PM2.5与环境气象条件的关系,表明本区域采暖期环境气象条件对PM2.5浓度影响显著。能见度越好、日照时间越长、气温越高,PM2.5浓度越小;风速越大、混合层高度越高,大气水平和垂直扩散能力越强,PM2.5浓度亦越小;而空气相对湿度越高、云量越多,PM2.5浓度越大。风速较大时一般混合层高度也较高,大气水平和垂直扩散能力均较强,PM2.5浓度较低。5mm以上连续性降水过程对PM2.5的净化效果明显,持续多日平均风速2.3m/s以上的较大风速过程也有很好的净化效果。2.0mm以下的单日降水在风速较小时净化效果不明显,1.0mm以下的微量降水在风速较小时还会使PM2.5浓度不降反升。     

长玻纤增强注塑聚醚醚酮复合材料加工工艺与力学性能的研究

以含30％的长玻璃纤维增强聚醚醚酮为原材料,采用注塑成型的方法研究了聚醚醚酮复合材料的加工工艺参数包括冷却速率、成型压力、成型温度及模具温度与力学性能的关系,并对模具温度为180℃时PEEK复合材料的微观形貌进行分析,研究结果表明：采用中速冷却速率,成型压力为120MPa,成型温度为后段375℃、中段425℃、前段425℃,模具温度保持为180℃时,复合材料的抗拉强度达81MPa、剪切强度为62．7MPa,制品表面光滑,其综合力学性能最佳。     

乳液聚合法制备纳米Al2O3/PS核壳式复合粒子

针对纳米粒子易团聚的特点,本文采用乳液聚合方法制备纳米Al2O3／PS复合粒子来进行改性,考察了不同工艺参数对乳液聚合的影响,并运用TEM、FTIR对复合粒子进行了表征。研究发现：在反应温度为800℃,乳化剂为$DS和OP—10复合乳化剂,St和纳米Al2O3投料比为2：1,单体滴加速度为5滴／min条件下所制备出的复合粒子具有以纳米驰03为核,PS为壳的核壳式结构,其包覆层厚度大约为10～20nm。     

直升机典型结构加速腐蚀试验方法研究

简要介绍了军用直升机的腐蚀现状及直升机结构加速腐蚀试验方法.对比分析了某型机典型试件中性+酸性盐雾试验及铜加速乙酸盐雾试验方法,探讨了铜加速腐蚀试验机理.试验结果显示:铜加速乙酸盐雾试验符合工况下腐蚀.     

机体/动力装置一体化分析中的动力影响效应数值模拟

采用合适的进、排气边界条件, 对带动力的单独涡扇发动机模型和带动力的DLR-F6翼身架舱复杂组合体(WBPN)模型的流场进行了数值模拟和分析.运用Roe三阶迎风偏置通量差分裂方法和隐式近似因子分解方法求解雷诺平均Navier-Stokes方程, 基于点搭接多块网格技术生成高质量计算网格, 通过多重网格技术来加速收敛.着重对动力发动机进、排气边界条件的给定进行了推导, 以准确地模拟发动机动力效应.计算结果与实验值吻合良好, 验证了所采用计算方法、网格分块策略和边界条件处理方法的正确性.      

一种保留几何及属性边界的网格简化方法

在实际应用领域,三维模型除包含由三角形网格构成的几何、拓扑信息外,还包含颜色、纹理、法矢量等属性信息,因此数据量较大,且不可避免地存在边界和孔洞.基于三角形折叠的方法,对误差矩阵的计算和误差控制方法进行了改进,并提出了几何及属性边界三角形的概念,给出了一种保留原始模型边界及属性信息的简化算法.该算法针对不同的边界情况将原始三角形网格划分为边界三角形、角点三角形、内部三角形及特征三角形,并采取相应的约束策略,在减小模型数据量的同时,较好地保留了边界和属性信息,并且生成递进网格文件,为包含属性的非封闭网格模型提供了连续多分辨率的模型重现.实验结果证明该方法快速有效,已成功应用于基于Web的三维递进传输和发布.      

武器装备环境适应性要求、环境适应性验证要求和环境条件及其相互关系的讨论（一）

文章分为两部分:第一部分论述环境适应性及其与可靠性的区别,环境适应性要求及其特点,探讨环境适应性的表征方法,介绍其在我国工程应用中存在的一些问题。第二部分论述环境适应性的验证要求,介绍目前型号中的“环境要求”、“环境技术要求”、“环境条件”等提法的实际含意和不足之处,并建议使用更为合理的名称;此外,通过分析装备环境适应性要求的类型和指标体系,给出了整个装备（整机）和下层产品的环境适应性指标体系框架和示例。此篇为第一部分。     

Timing and sex effects on the “Spatial Orientation Test”: A World War II map reading test

The present study aimed to document the psychometric properties of a recently declassified map reading test used in World War II, known as the Spatial Orientation Test (SOT), which measures mostly the ability to match map and aerial images. We also examined the influence of timing conditions and sex of the participants as correlates of performance. A total of 101 participants (41 males, 60 females) completed the SOT, along with other spatial tests and spatial affect scales (tapping spatial anxiety and confidence). Results showed a significant male advantage on this rediscovered map reading test. Additionally, timing affected overall performance but not the magnitude of sex differences. Finally, significant correlations were found between the SOT and other spatial tests and scales. The processes underlying this test and its potential for future use are discussed.     

旋翼三维非定常跨音速绕流的数值模拟

 利用小扰动位势方程，用有限差分方法求解了旋翼跨音速流场。导出了严格的三维非定常位势方程远场无反射边界条件，并成功地用于数值计算中，缩小了物理求解域的空间尺度。采用了贴体坐标和网格加密技术，以得到合理的非均匀网格分布。应用较少的网格点数成功地计算了无升力情况下旋翼的三维非定常亚、跨音速绕流流场，得到了与实验结果符合良好的数值解     

The effect of inlet conditions on the flow and heat transfer in multiple rotating cavity with axial throughflow

This paper discusses experimental results from two different build configurations of a heated multiple rotating cavity test rig.Measurements of heat transfer from the discs and tangential velocities are presented.The test rig is a 70% full scale version of a high pressure compressor stack of an axial gas turbine engine.Of particular interest are the internal cylindrical cavities formed by adjacent discs and the interaction of these with a central axial throughflow of cooling air.Tests were carried out for a range of non-dimensional parameters representative of high pressure compressor internal air system flows(Re up to 5×106 and Rez up to 2×105).Two different builds have been tested.The most significant difference between these two build configurations is the size of the annular gap between the(non-rotating) drive shaft and the bores of the discs.The heat transfer data were obtained from thermocouple measurements of surface temperature and a conduction solution method.The velocity measurements were made using a two component,LDA system.The heat transfer results from the discs show differences between the two builds.This is attributed to the wider annular gap allowing more of the throughflow to penetrate into the cavity.There are also significant differences between the radial distributions of tangential velocity in the two builds of the test rig.For the narrow annular gap,there is an increase of non-dimensional tangential velocity V/Ωr with radial location to solid body rotation V/Ωr=1.For the wider annular gap,the non-dimensional velocities show a decrease with radial location to solid body rotation.