含弹内埋弹舱缩尺模型气动噪声特性研究

目的对含弹的内埋弹舱模型进行噪声仿真和试验研究。方法计算采用"CFD+CAA"的混合方法,采用DDES计算流场,基于M?hring声学类比方法得到测量点的噪声信息。采用该方法与空腔M219标准试验结果进行对比。内埋弹舱吹风试验在全消声室中进行,并采用传声器阵列识别主要噪声源。结果计算与试验得到的不同来流条件下,不同测量点的噪声频谱曲线基本一致。弹舱内最大声压级出现在中间弹翼附近的侧壁上,与声源识别的主要噪声源的位置一致。结论该研究可为内埋弹舱的设计提供参考和技术支持。     

陆架浅海沉积物-海水界面溶质通量的计算方法及其应用

陆架浅海沉积物—海水界面上的溶解态生源物质通量的准确估算是海洋生态系统动力学研究中的关键性问题之一。由于底栖生物活动以及海流、海浪及潮波与海底地形地物相互作用的影响 ,使得该通量的准确估算十分困难。本文综合分析讨论了近年来提出的各种计算该类通量的物理模型及参数的确定方法 ,并结合在中国黄、东海等陆架浅海水层—底栖生态动力学耦合模型研究的需要 ,比较深入地讨论了应用过程中应该考虑的几个问题     

制动器用电磁体的另一种非对称磁路设计

为了获得更好地制动安全性及延长制动器寿命,针对相关文献中制动器用电磁体磁路的非对称设计方案的不足之处,提出了新的磁路形状设计,即采用开槽的方法来获得要求的非对称磁路,并对此作了理论分析。由于磁路形状复杂,采用Ansoft软件中Maxwell-3D对设计的电磁体进行磁场及其吸力的仿真计算。对仿真结果和理论分析作了对比。以此制作的样品试验结果表明,电磁体工作姿态平稳,未发现因卡死而出现摩擦力的大幅度波动。且磨损均匀,满足了工作寿命的相关要求,为电磁制动器安全制动、延长工作寿命提供了保证。     

我国油气企业环境会计核算及信息披露的探讨

在国民经济中占有主导地位的油气企业同时也是造成环境污染的主体之一。因此,建立油气企业环境会计制度有极其重要的现实意义。文章针对我国油气企业环境会计制度应用现状,运用环境会计基本理论,对企业环境会计核算方法及信息传播模式进行了探讨,以期为油气企业环境会计制度的实施提供一些理论依据和具体方法,推动油气企业环境会计制度的发展。     

计算流体力学(CFD)中的迭代法及其并行计算方法

应用计算流体力学 (CFD)方法分析事故原因已被广泛采用 ,笔者针对事故理论分析和流体计算过程中 ,运用CFD方法所存在计算量大的问题 ,分析和讨论了几种古典迭代法及其并行计算方法     

基于模糊颜色Petri网的表决DVP安全软件模型初探

把模糊计算理论和有色Petri网有机地结合起来 ,提出了一种模糊颜色Petri网诊断表决算法 ,把该算法应用于DVP的软件模型 ,使之具有故障容忍和表决的能力。笔者对以模糊颜色Petri网为核心的DVP软件模型表决算法进行了较为深入的探讨 ,该模型对提高软件系统的安全性和可靠性具有实际意义。     

STABILITY AND REACH LENGTH IN WATER SURFACE PROFILE DETERMINATION1

ABSTRACT: Extension of basic step methods of backwater computation to reaches of finite length is examined. Accuracies of commonly accepted hydraulic loss equations under particular water surface profile conditions are compared. Simulation of energy lines within a reach by parabolic curves is found to minimize error provided orientation of the axis of the parabola is selected in accordance with prevailing hydraulic conditions. Theoretical basis for an index reach length beyond which single-step computation from end to end of the reach must be in error is developed. Reduction of this reach length by suitable factors tailored to hydraulic conditions yields a mathematically defined allowable reach length for backwater computation. When reach length does not exceed this allowable reach length, no significant error may be detected. Automatic insertion of synthetic cross sections interpolated between surveyed cross sections when these are inadvertently spaced too far apart enables computation to proceed. This device is error-free for prismatic channls but may introduce error for irregular natural channels. Preliminary trials indicate that results so obtained may be accepted provided the fall in the original reach does not exceed from one to two feet. When this is exceeded, additional cross sections should be surveyed.     

WATER BUDGET COMPUTATION FOR A SHALLOW LAKE-LAKE OKEECHOBEE,FLORIDA1

ABSTRACT: The water budget computation in shallow lakes is complicated because marsh vegetation can transpire large quantities of lake water. Thus, a model including the marsh zone evapotranspiration (WET) was developed to compute the water budget for Lake Okeechobee. Three periods of testing (1969–74), planning (1963–74), and recorded period (1952–77) were used to compare the differences of the sum of storage deviation between the WET and conventional methods (WOET). Results of the WOET method showed that the sum of stage deviations were 87.42 cm (2.868 ft.), 231.80 cm (7.605 ft.), and 284.50 cm (9.333 ft.) in the testing, planning, and recorded periods, respectively. These stage deviations are equivalent in the same order to 29, 76, and 93 percent of the lake volume. In general, the WET method not only was applicable to compute the water budget for the lake but also reduced the sum of storage deviation by about 42, 31, and 49 percent, respectively, in those three periods. The storage deviation in WET method was reduced on an average to about 2 percent each year in all three periods, and the deviations were scattered more randomly than in WOET.     

空调压缩机冷媒爆炸反应特征分析

冷媒与空气的反应特征对空调压缩机安全性有重要影响.本文采用最小自由能原理,分别对两种冷媒R407C和R410A与空气的混合气体的爆炸反应参数进行了数值计算,得到了不同初始压力和不同冷媒含量条件下,混合气体爆炸反应温度和压力,分析了混合气体反应压力条件和爆炸极限范围.结果表明:初始压力低于0.2 MPa时,R407C-空气混合气体和R410A-空气混合气体均不会发生爆炸;初始压力超过0.3 MPa时,混合气体能够发生爆炸,爆炸反应温度和压力随着初始压力的升高而升高;R407C和R410A质量分数分别在34%、35%左右,混合气体反应温度和压力达到最大值.R407C和R410A易燃易爆特征相近;但爆炸范围都比氟利昂(R22)气体宽,即同样的条件下更容易发生爆炸.该计算结果能够为新型冷媒R407C和R410A的安全使用提供一定的依据.     

平纹滤布除尘性能的研究

从织物的结构来分析过滤的机理,推导出颗粒通过滤布的理论计算式,并用实际滤布作试验来验证该计算式的可靠性。