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611.
从面向对象的程序设计的角度,剖析了CLIENT/SERVER环境下的通用数据库开发工具POWERBUILDER(PB)的特点、基本结构及其开发数据库应用系统的方法。 相似文献
612.
在算子单调性和紧性假设下研究了半线性算子方程f∈Au-Tu+cu的可解性,其中A,T和C映一个自反Banach空间X的子集到它的对偶空间。所得结果扩展或改进了Guan最近的结果。 相似文献
613.
以某高射机枪为研究对象,采用有限元法对该枪进行建模,并用实验研究的结果检验和修改了理论模型。计算了该枪的结构动态特性和枪口动力响应,从改善射击精度的角度出发,通过对若干结构修改方案的模拟计算,提出了该枪结构修改的参考意见。 相似文献
614.
应用MSD—3O—S逆变电源及普通刷镀电源,研究了脉冲刷镀层的沉积速度、硬度、耐磨性、结合强度等方面的性能,并与直流刷镀层进行了比较,结果表明脉冲刷镀层性能优于直流刷镀层。 相似文献
615.
基于少齿差传动的高精度方向机研究 总被引:1,自引:0,他引:1
目前大多数坦克炮塔方向机均采用一行星汇流排将手动与电动合二为一.但由于受到结构及坦克空间约束,方向机的传动比基本上均匀分配,系统各级精度均对系统误差产生影响,因而空回量大、传动精度低,通常在2.5密位以上.本研究通过采用"同力面混合少齿差行星传动"技术及径向弹性补偿装置,并对系统各级传动比重新分配,使方向机的空回量约减小一半,提高了方向机的传动精度和传动效率. 相似文献
616.
给出了偏心加筋板大变形分析的理论公式和相应的梁板单元模型 .在肋骨和板的运动方程中引用 Von Karman形变方程 ;按照 Mindlin板理论计及横向剪切变形的影响 ;对横向剪应变和薄膜应变重新插值修正克服 Mindlin型单元在薄板应用时的“锁定”行为 ,此模型可适合于薄板和厚板的非线性分析 . 相似文献
617.
对模拟转子进行了不平衡响应的有限元计算,并进行了相应的实验研究.在转速为960r/min和1568r/min时,不平衡响应的计算结果与实验结果的误差近似为1.7%和2.1%,计算结果与实验结果相符. 相似文献
618.
David R. Morrison Jason J. Sauppe Wenda Zhang Sheldon H. Jacobson Edward C. Sewell 《海军后勤学研究》2017,64(1):64-82
The cyclic best‐first search (CBFS) strategy is a recent search strategy that has been successfully applied to branch‐and‐bound algorithms in a number of different settings. CBFS is a modification of best‐first search (BFS) that places search tree subproblems into contours which are collections of subproblems grouped in some way, and repeatedly cycles through all non‐empty contours, selecting one subproblem to explore from each. In this article, the theoretical properties of CBFS are analyzed for the first time. CBFS is proved to be a generalization of all other search strategies by using a contour definition that explores the same sequence of subproblems as any other search strategy. Further, a bound is proved between the number of subproblems explored by BFS and the number of children generated by CBFS, given a fixed branching strategy and set of pruning rules. Finally, a discussion of heuristic contour‐labeling functions is provided, and proof‐of‐concept computational results for mixed‐integer programming problems from the MIPLIB 2010 database are shown. © 2017 Wiley Periodicals, Inc. Naval Research Logistics, 64: 64–82, 2017 相似文献
619.
As a main oxidizer in solid composite propellants, ammonium perchlorate (AP) plays an important role because its thermal decomposition behavior has a direct influence on the characteristic of solid com-posite propellants. To improve the performance of solid composite propellant, it is necessary to take measures to modify the thermal decomposition behavior of AP. In recent years, transition metal oxides and carbon-supported transition metal oxides have drawn considerable attention due to their extraor-dinary catalytic activity. In this review, we highlight strategies to enhance the thermal decomposition of AP by tuning morphology, varying the types of metal ion, and coupling with carbon analogue. The enhanced catalytic performance can be ascribed to synergistic effect, increased surface area, more exposed active sites, and accelerated electron transportation and so on. The mechanism of AP decom-position mixed with catalyst has also been briefly summarized. Finally, a conclusive outlook and possible research directions are suggested to address challenges such as lacking practical application in actual formulation of solid composite propellant and batch manufacturing. 相似文献
620.
He-yang Xu Wei-bing Li Wen-bin Li Qing Zhang Ya-jun Wang Xiao-wen Hong Ying Yang 《防务技术》2021,17(5):1650-1659
The failure mechanism of a cylindrical shell cut into fragments by circumferential detonation collision was experimentally and numerically investigated. A self-designed detonation wave regulator was used to control the detonation and cut the shell. It was found that the self-designed regulator controlled the fragment shape. The macrostructure and micro-characteristics of fragments revealed that shear fracture was a prior mechanism, the shell fractured not only at the position of detonation collision, but the crack also penetrated the shell at the first contact position of the Chapmen-Jouguet (C-J) wave. The effects of groove number and outer layer thickness on the fracture behavior were tested by simulations. When the thickness of the outer layer was 5–18 mm, it has little effect on fragmentation of the shell, and shells all fractured at similar positions. The increase of the groove number reduced the fracture possibility of the first contact position of the C-J wave. When the groove number reached 7 with a 10 mm outer layer (1/4 model), the fracture only occurred at the position of detonation collision and the fragment width rebounded. 相似文献