Decoration of disclinations by solidification-induced band texture and focal-conic texture for a low-molar-mass liquid crystal

Two decoration techniques, solidification-induced band texture decora tion and focal-conictexture decoration, have been established to exhibit the director field of disclinations in a low-molar-mass methacrylate liquid crystal. The disclinations with strength s = 1/2 and s = ±1 are observed by the two decor ation methods. For the solidification-induced band texture decoration, the molecular orientation is perpendicular to the direction of the band. While for focal- conictexture decoration, it has been proved by the results of IR dichroism that the direction of the director is parallel to the direction of the focal-conic. Therefore, the sketch map of the molecular director filed can be mapped according to the morphological pattern of the solidification-induced band textureor focal-conic texture.     

关于浮力场概念的引入及其P的力能二重性

在一个均匀且连续充满整个空间的静止液体中引入伴随重力场而存在的浮力场概念,通过它的场力做功揭示其P的力能二重性,进而把浮力场概念推广到液体(理想)的稳定流场中,并以新的观点和方法推导出液体(理想)作稳定流动的一系列重要定理、定律.对于进一步认识浮力本质及其应用有着重要意义.     

催化电位法测定人发中痕量碘

采用碱灰化法消解发样,于中性溶液中离心去除杂质,在酸性溶液中以催化电位法测定发碘含量,回收率达98.6％;变异系数(CV)为8.7％;测出中碘地区一个教学班20名男学生发碘平均含量为0.93μg/g,与文献报道相近。     

298K毛吸附溴化烷基三甲铵的性质及自由能

用液 /固吸附计量置换模型 ( SDM- A) ,研究了 2 98K羊毛纤维吸附溴化烷基三甲铵阳离子表面活性剂 CTAB和 DTAB的吸附等温线 ,结果表明它们均遵从 SDM- A的线性作图关系 .用 SDM-A的线性参数βα 和 q/z很好地描述了碳氢链长及加盐效应对于吸附性质的影响规律 ,特别是能定量地描述加盐效应对于吸附同时具有的促进和抵消两种相反作用的程度 ,并用 SDM- A的热力学 ,由线性参数计算得到了不同体系的吸附亲和能 ΔGA,解吸能 ΔGD 及总过程的自由能 ΔGP.一个吸附体系中 ,ΔGA 为常数且为较大的负值 ;ΔGD 为随溶液体相浓度 c增大而增大的正值 ;ΔGP为与 lgc呈线性关系的较小的负值 .计算所得结果能很好地解释实验事实 ,并可从更深层次上揭示吸附机理 .     

液压传动系统设计中的几个关键问题

文章分析研究了液压传动系统设计中的几个关键性问题。     

烟气分析在转炉冶炼过程中的应用研究

介绍转炉烟气分析控制系统,研究转炉烟气和炉气在冶炼过程中的变化规律,并开发烟气定碳模型。结论表明,在转炉冶炼过程中利用烟气成分的变化规律,可进行转炉炉况判断、终点判断和了解炉内反应过程。开发的烟气定碳模型对于含碳量低于0.12%的炉次,其控制精度为±0.02%,命中率为90%。     

乳化液膜法净化湿法磷酸除镁研究

采用乳化液膜技术对湿法磷酸进行脱镁净化是一种净化湿法磷酸的新途径。采用正交试验设计方法组织实验，结果表明在实验研究范围内，萃取剂对湿法磷酸中脱镁效果有高度显著的影响，而表面活性剂、膜试剂和反萃取剂对镁的脱除有一定影响。     

层流液柱吸收法测定气体在液相中的扩散系数

采用射流吸收的简捷方法，通过测定由Ｓｈｏｕｔｈｗｅｌｌ型孔板所产生的截面速度均匀的层流喷射液柱所吸收的气体量，由渗透理论所导出的模型，可计算出一定温度、压力下的微溶气体在液相中的分子扩散系数Ｄ。在温度为３０～４５℃的范围，测试结果与文献值吻合良好．     

The detection of structural deformation errors in attitude determination

In the determination of the attitude parameters from a multi-antenna GPS array, one of the major assumptions is that the body frame is rigid at all times. If this assumption is not true then the derived attitude parameters will be in error. It is well known that in airborne platforms the wings often experience some displacement during flight, especially during periods of initializing maneouvres, such as taking off, landing,and banking. Often it is at these points in time that it is most critical to have the most precise attitude parameters.There are a number of techniques available for the detection of modeling errors.The CUSUM algorithm has successfully been implemented in the past to detect small persistent changes. In this paper the authors investigate different methods of generating the residuals, to be tested by the CUSUM algorithm, in an effort to determine which technique is best suited for the detection of structural deformation of an airborne platform. The methods investigated include monitoring the mean of the residuals generated from the difference between the known body frame coordinates, and those calculated from the derived attitude parameters. The generated residuals are then passed to a CUSUM algorithm to detect any small persistent changes. An alternative method involves transforming the generated residuals into the frequency domain through the use of the Fast Fourier Transform. The CUSUM algorithm is then used to detect any frequency changes. The final technique investigated involves transforming the generated residuals using the Haar wavelet. The wavelet coefficients are then monitored by the CUSUM algorithm in order to detect any significant change to the rigidity of the body frame.Detecting structural deformation, and quantifying the degree of deformation, during flight will ensure that these effects can be removed from the system, thus ensuring the most precise and reliable attitude parameter solutions. This paper, through a series ofsimulations, will assess the effectiveness of the above mentioned techniques for detecting structural deformation effects on a GPS multi-antenna array. These principles are then tested with experimental data.