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基于labview的汽车尾气检测系统研究 总被引:1,自引:0,他引:1
针对汽车尾气排放污染物检测要求,通过面向对象的软件编程技术及可视化的编程语言Visual C++,以labview软件为平台,运用动态链接库,首次设计出针对不同车型的汽车排放污染物检测系统.该系统实现了数据的输入输出,检测参数的采集,数据的分析和处理等功能.对系统进行了简单的试验和结果分析,证明该系统功能全面,界面直观,易操作,实用性强. 相似文献
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左伟 《西安航空技术高等专科学校学报》2009,27(5)
分析了国内外精密电铸铜发展现状,提出了电流和添加剂对电铸层表面形貌的影响,以及铸液中添加剂的存在对基质金属铜的晶粒有明显的细化作用.使电铸层的显微硬度、耐磨性及抗拉性有明显提高. 相似文献
315.
A Self-organizing Bearings-only Target Tracking Algorithm in Wireless Sensor Network 总被引:1,自引:0,他引:1
In the bearings-only target tracking, wireless sensor network (WSN) collects observations of the target direction at various nodes and uses an adaptive filter to combine them for target tracking. An efficient network management is necessary to gain an optimal tradeoff between locating accuracy and energy consumption. This article proposes a self-organizing target tracking algorithm to select the most beneficial subset of nodes to track the target at every snapshot. Compared with traditional methods, this scheme avoids the need for keeping global position information of the network as in greedy selection. Each node judges its future usefulness depending on the knowledge of its own position and using simple mathematics computation. Simulations indicate that this scheme has locating accuracy comparable to the global greedy algorithm. Also, it has good robustness against node failure and autonomous adaptability to the change of the network scale. Furthermore, this algorithm consumes limited energy because only a portion of nodes partakes in the selection at every snapshot. 相似文献
316.
Yang Wei-hua Cao Jun Shi Rui Hao Xu-sheng Song Shuang-wen 《Acta Astronautica》2011,68(11-12):1782-1789
A new series of test pieces with different geometrical configuration and geometry dimensions are designed to experimentally investigate on impingement-effusion cooling behavior in curve effusion wall of combustion chamber. The test results show that the discharge coefficient increased with the increasing blowing ratio. The effusion hole–hole spacing has an effect on the discharge coefficient and the discharge coefficient commonly decreased with the increment of effusion hole–hole spacing. The blowing ratio greatly effects cooling behavior. The bigger blowing ratio is favorable for improving cooling characters. At the curved effusion wall, to begin with, cooling effectiveness increased slowly and kept a steady value in subsequence. But, for the rear end of curved effusion wall, it decreased slowly. With decreasing of effusion hole angle and effusion hole–hole spacing, cooling effectiveness is enhanced. Meanwhile, blowing ratio, effusion angle and effusion hole–hole spacing take an evident effect on the discharge coefficient. 相似文献
317.
通过对计划和规划概念上的比较分析,对市场经济条件下规划存在的必要性进行了探讨,并给予了肯定回答.在市场经济条件下规划具有经济宪章、促进经济社会协调发展、遏制政府失灵、构建经济伦理四个方面的作用,从而为规划作为宏观管理的重要手段建立了一个有解释力的逻辑框架. 相似文献
318.
Rui Tu Li Wang 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2014
A method of real-time coseismic wave retrieving was proposed based on the tight integration of GPS, Glonass and strong-motion sensor observations, the validation and precision analysis have been made by an experimental data. The series of results have been shown that: by the integrated Kalman filter and multi-sensors, the coseismic waves can be optimally recovered by complement the advantages of each other, especially when the observation conditions are very bad. In additional, the results are not significantly effected by different receiver clock error processes for the integration solution. 相似文献
319.
The application of computational fluid dynamics/computational solid method (CFD/CSM) on solving the aero-thermo-elastic problem of spinning rocket is introduced. Firstly, the aerodynamic coefficients of a rocket are calculated, and the results are compared with the available experimental data, which verified the accuracy of the CFD output. Then, analysis is carried using ANSYS Workbench multi-physics coupling platform, which includes fluid, thermal, and structural solvers. The results show that spinning causes a significant effect on the de formations and stresses. Furthermore, thermal stresses due to high temperature at the rocket warhead and tail edges have a dominated effect, even more than those produced by aerodynamic forces. Consequently, this important outcome should be taken into consideration during the rocket design stages. 相似文献
320.