水轮机水力稳定性的分析

根据收集国内外水轮机水力稳定性资料 ,分析了引起水轮机水力不稳定性的因素 ,并结合实例分析可能引起的危害 ,最后提出了解决问题的方法和建议     

INVESTIGATION ON OVERCOMING WEFT DETWISTING AIR-INSERTION OF AIR-JET LOOM

A special tip of vortex twisting nozzle is designed and fastened at the exit out of the drafted reed space or shed. Compressed air is supplied by the tube near the last subnozzle, weft yarn is retwisted and twistloss can be totally compensated with slight excess of 0.74%.     

稀土永磁同步电机的电枢反应理论及合群漏磁

本文分析了稀土永磁同步电机直轴电枢反应。主要分析了负载时由直轴电枢反应引起的漏磁通,其中包括合群漏磁和“曾氏漏磁”,并推导了这些漏磁通的定性计算公式,完善了永磁同步电机的电磁设计计算。     

双门电冰箱的热传导问题

本文将根据热传导方程,对电冰箱达定态过程进行理论推导,以及定态后电冰箱单位时间吸收的热量,并由此计算出由于冰箱箱体的热量泄漏而消耗的能量。     

新型压电陶瓷涡街流量计

介绍一种新型的压电陶瓷涡街流量计,该流量计采用ＢＳＴ压电陶瓷元件来检测旋涡释放频率,使该流量计能在高温工况下工作,一年多的工业现场运行试验结果表明,新研制的涡街流量计可靠性高、稳定性好,在４００℃高温和１０ＭＰａ高压下能长期连续正常运行。     

前向多翼离心风机叶片尾迹和蜗壳二次流动的试验研究

对前向多翼式离心风机建立了性能及流场测试台位 性能试验及流场测试表明,性能试验重复性良好,曲线符合理论性能曲线.用粒子图像速度场仪技术对叶片尾迹区及蜗壳出口横截面上的二次流做了详细的变工况测量与分析.结果表明:叶片尾迹区脉动强度达20%～70%;在设计工况附近叶片尾迹影响区域小,在非设计工况下叶片尾迹影响区域大,尾迹区域占到蜗壳径向宽度的15%～25%,约是叶片弦高的2～3倍;在蜗壳横截面上明显存在二次流旋涡;沿着蜗壳旋出方向二次流对称分布,但是到达出口时,小流量下两侧旋涡结合成一个旋涡,大流量下两侧旋涡一直保持到蜗壳出口.     

BiCrO3薄膜的溶胶-凝胶制备方法

用溶胶-凝胶方法在LaNiO3／Si衬底上在450℃退火条件下制备了BiCrO3.薄膜XRD研究发现BiCrO3仅有少量结晶，呈（I0I）择优取向．铁电性测试表明，室温下薄膜具有铁电性，剩余极化强度为0．6μc／cm^2，漏电流研究表明薄膜的导电机构分为三种。     

在中空纤维膜中Dean涡降低浓差极化的试验研究

膜污染与浓差极化是不同的概念，两者是相互关联、相互影响的，浓差极化使膜表面被截留组分浓度提高，从而加速了膜污染过程的，而膜污染使部分膜孔堵塞，又会促使局部浓差极化的加剧．因而，膜污染与浓差极化成因果关系，浓差极化是导致膜渗流量下降和分离效率降低的原因．在中空纤维膜中，Dean涡这种不稳定流能有效地将膜靠近膜壁的浓差极化现象大大消除．通过设计一组试验，证明了浓差极化的危害性和Dean涡能较大程度的降低浓差极化．从能耗的观点上说，试验结果表明，有Dean涡存在的编织型中空纤维膜，其能耗低于直线型，其渗透流量和回收率高．图12．参19．     

基于子波变换的消噪方法在涡街流量传感器中的应用

基于子波变换消噪原理，结合流量测量持定要求，提出了一种适用于在涡街流量传感器信号处理的单支重构滤波方法，同时给出了滤波级数的选取方法，这种计数方法能够有效地扩大涡街流量传感器的量程下降，通过对实际信号的分析，证实了方法的有效性。     

Instability of the shear layer in the near wake of a circular cylinder

The instability of the shear layer separated from a circular cylinder is studied with the Reynolds number (Re) of 3000～104 by numerically solving the two-dimensional Navier-Stokes equations. In the wake of the cylinder, primary vortex shedding with natural frequency fs occurs, and the instability of the shear layer with frequency ft develops, which leads to mixing layer eddies and interacts with the primary shedding vortices. However, there remains some uncertainties regarding to the variation of the shear layer characteristic frequency with the Reynolds number. Based on the previous experimental work, several relationships of ft/fs with Re has been proposed including ft/fs～Re0.5 by Bloor, ft/fs～Re0.87 by Wei and Smith and ft/fs～Re0.67 by Prasad and Williamson. The objective of this study is to predict reasonably the relation of the shear layer instability frequency with the Reynolds number based on the present accurate calculation with the high-order schemes and high-resolution spectrum analysis. According to our calculated results, a variation for the normalized shear-layer frequency of the form ft/fs～Re0.69 is predicted numerically, which is in good agreement with a recent experimental measurement of Re0.67 and physical prediction of Re0.7.