BEPCII直线注入器的尾场效应

BEPCII直线注入器中的强流、短束团的尾场效应将损害束流的性能.用分析解和数值模拟计算的方法,系统地研究了尾场对纵向和径向束流动力学的影响,包括单束团的短程尾场和多束团的长程尾场对束流能量、能散、发射度、轨道和初级电子束在正电子产生靶上束斑尺寸的影响等.研究了有效抑制这些尾场效应的措施     

三氯乙烯有致癌作用

 2006年7月,加拿大国家研究委员会(NationalResearchCouncilCanada,NRC)做出结论,认为有足够的科学依据证实三氯乙烯(trichloroethylene,TCE)会对人体健康造成危害。2001年,美国环保署(Environ-mentalProtectionAgency,EPA)已针对三氯乙烯发表了一份评估报告草案。报告含蓄地指出,目前遍布美国的军事和制造业基地都广泛地以三氯乙烯为脱脂剂进行清洁和洗涤,而对这些地区的三氯乙烯污染进行治理,预计需花费数十亿美元。     

基于积分方法的二维平行剪切层声远场预测

本文采用二维Ffowcs Williams＆Hawkings(FW-H)方程对平行剪切层远声场辐射特性进行了研究。近流场时间精确数据通过计算气动声学(Computational Aeroacoustics,CAA)技术数值模拟获得,声远场信息则通过FW-H方程对近流场内的可穿透积分面进行积分获得。该方法首先采用具有解析解的涡/尾缘干涉问题进行了校核,进一步采用CAA/FW-H匹配技术对二维平行剪切层声辐射问题进行了预测,计算结果表明,积分解与计算域内的CAA数值解吻合较好。     

水溶液中痕量游离氯的气动电流法测定

气动电流法是适用于水溶液中痕量溶质分析的一种新方法。在试样被酸化的同时,通过氮气使游离氯转入气相,并在覆膜电极检定器上还原为Cl~-加以测定。检定池的电解质为9NH_2SO_4。厚0.5-Mil的聚四氯乙烯膜由表面粗糙化和用聚合物质处理以后,覆膜电极检定器的电流响应一般增加100倍以上。使用处理过的膜其寿命可达六个月。游离氯的检定极限在2ml试样中估计为1.0μg     

微量元素缺乏症及其防治

报道了以235名健康小儿的血清锌、铜正常参考值及铜／锌比值作依据，对538名本地区集体儿童进行了调查．对240例不同病种患儿的血清锌、铜含量测定，并进行了分析；对G6PD、GSH-PX、AKP醇活性与微量元素含量的关系进行了相关性比较；对微量元素锌缺乏症的患儿进行了临床治疗观察；对微量元素缺乏症的防治进行了讨论．     

微波等离子体炬发射光谱法去溶系统性能的研究

用微波等离子体矩（MPT）作激发光源，等离子体的工作气体为氩气，研究了气动雾化进样去溶系统的工作参数对分析性能的影响，探讨了水冷凝与浓硫酸吸收二者协同去溶的相关性，结果表明，OH （Q1带，带头谱线为308.520nm）的发射强度即可判别样品去溶效果。     

Influences of aerodynamic loads on hunting stability of high-speed railway vehicles and parameter studies

The influences of steady aerodynamic loads on hunting stability of high-speed railway vehicles were investigated in this study.A mechanism is suggested to explain the change of hunting behavior due to actions of aerodynamic loads：the aerodynamic loads can change the position of vehicle system（consequently the contact relations）,the wheel/rail normal contact forces,the gravitational restoring forces/moments and the creep forces/moments.A mathematical model for hunting stability incorporating such influences was developed.A computer program capable of incorporating the effects of aerodynamic loads based on the model was written,and the critical speeds were calculated using this program.The dependences of linear and nonlinear critical speeds on suspension parameters considering aerodynamic loads were analyzed by using the orthogonal test method,the results were also compared with the situations without aerodynamic loads.It is shown that the most dominant factors a ff ecting linear and nonlinear critical speeds are different whether the aerodynamic loads considered or not.The damping of yaw damper is the most dominant influencing factor for linear critical speeds,while the damping of lateral damper is most dominant for nonlinear ones.When the influences of aerodynamic loads are considered,the linear critical speeds decrease with the rise of cross wind velocity,whereas it is not the case for the nonlinear critical speeds.The variation trends of critical speeds with suspension parameters can be significantly changed by aerodynamic loads.Combined actions of aerodynamic loads and suspension parameters also a ff ect the critical speeds.The effects of such joint action are more obvious for nonlinear critical speeds.     

低空大展弦比无人机翼梢磁梯度测量探头气动特性及影响

针对一种低空大展弦比无人机, 文章进行全机和翼梢磁梯度测量探头数值模拟.全机计算给出翼梢磁梯度测量探头对全机气动特性和操稳特性的影响; 翼梢磁梯度测量探头计算实现了气动外形优化设计, 在保持全机操稳特性的前提下, 最大程度地减小全机气动阻力增量.结果表明, 磁梯度测量探头对全机气动阻力增量在9%之内, 俯仰力矩变化在5%之内, 对全机操稳特性的影响不大, 气动外形优化设计基本满足该低空大展弦比无人机的安全飞行技术要求.