动力学涂层毛细管电泳分离双链脱氧核糖核酸片段

以异丙醇为聚合反应链转移试剂，水相法合成了短链聚N，N－二甲基丙烯酰胺（PDMA），研究表明，该聚合物能在毛细管内壁形成稳定的动力学涂层，从而有效地抑制电渗流和毛细管内壁与DNA的作用。这种介质被成功地应用于DNA片段的高效分离。     

CeO2对等离子喷涂Al2O3涂层抗热震性的影响

研究了不同含量ＣｅＯ２添加剂对等离子喷涂Ａｌ２Ｏ３涂层抗热震性能的影响。结果表明，添加适量的ＣｅＯ２，涂层中会形成细小网状微裂纹，这些微裂纹具有释放涂层应力的作用。ＣｅＯ２的加入起到阻碍αＡｌ２Ｏ３向γＡｌ２Ｏ３转变的作用，并可细化涂层组织、降低涂层中的孔洞数量，因而提高了涂层的抗热震性能。     

金属载体催化剂的涂层研究

在高温氧化处理不同时间的金属载体箔片上涂覆MgAl2O4/Al2O3过渡涂层,利用TG-DSC,XRD,SEM,BET和超声振动等分析测试技术,对载体和涂层的微观结构与表面特性进行研究.结果表明,在950 ℃下高温氧化5 h,箔片表面生成板状Al2O3晶须,有利于增强涂层与箔片的附着力.在载体表面涂覆一层MgAl2O4/Al2O3过渡涂层,有助于提高活性组分与金属载体的结合力,可以获得高结合强度的涂层结构,促使活性元素高度分散.     

聚合物涂层在毛细管电泳分离蛋白中的研究进展

毛细管电泳具有分析时间短,分离效率高,样品消耗量少等优点,在生物样品分离,特别是蛋白质分析领域有重要应用。然而,毛细管内壁硅羟基的解离给分离结果带来诸多不良影响。聚合物涂层能够抑制蛋白质在毛细管内壁的吸附以及调控电渗流,故对毛细管内壁进行有效修饰能够提高其对蛋白质的分离效率及分离稳定性。该文主要综述了动态及静态聚合物涂层毛细管的最新研究进展,并概述了近些年基于多巴胺/聚多巴胺发展起来的涂层毛细管的研究进展,最后展望了聚合物涂层毛细管的发展趋势。     

CeO2添加剂对等离子ZrO2涂层抗热震性的影响

在ZrO2陶瓷涂层中加入适量的CeO2，使陶瓷涂层的抗热震性能得到提高，这主要是由于CeO2的加入，涂层的微小孔隙增加、涂层产生细微的网状裂纹，增加了微裂纹密度，从而降低了徐层的弹性模量，释放了涂层中的应力，提高了涂层的裂纹失稳扩展时的临界温差ΔTc，并可阻止裂纹沿单方向的快速扩展，使涂层的抗热震起裂性能和抗热震失效能力得到提高。其中，CeO2加入量为9％效果最佳，过量加入CeO2，会过早地促进裂纹的扩展、断裂，不利于提高涂层的抗热震性能。     

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.     

基于遗传算法的升力体外形优化设计

升力体由于低热流率再入物理特性和高效的内部容积利用率，是高超声速飞行器气动外形的一种典型布局.文章对升力体飞行器进行参数化数值建模，并提取其表征外形的参数作为设计变量，综合考虑飞行器再入过程中的气动力、气动热、容积利用率及稳定性等性能指标.运用多目标混合遗传算法对升力体进行了多变量、多约束下的气动外形优化设计，获得了再入飞行器外形的最优Pareto解.数值模拟结果表明，典型状态下最优Pareto解与CFD结果相差12%，验证了优化结果的准确性.      

“组装法”证明对称不等式

随着科技的进步,如今大型桥梁、地铁等都是采用分段施工、整体合拢的“组装”建造模式.其实,在解决数学问题时,尤其是证明那些外形结构相似的对称(或对称轮换)不等式,也可以借鉴上述模式:先精心分割成对称的局部,紧盯整体的目标和方向,最后有机融合于一体,我们把这种方法称为“组装法”.1.几个案例