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631.
Tong Xu Yanli Hu Jian Wu Zhensen Wu Chunbin Li Zhenwen Xu Yucheng Suo 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2011
The seismo-ionospheric coupling is a hot topic of modern scientific research. One of the most reasonable mechanisms is the hypothesis of quasistatic electric field. With a preliminary analytical method, electric field in F2-region before Wenchuan earthquake was derived from the five lower latitude ground-based ionosondes: Lhasa (29.63°N, 91.17°E), Chongqing (29.50°N, 106.40°E), Kunming (25.00°N, 102.70°E), Guangzhou (23.15°N, 113.35°E) and Haikou (23.15°N, 110.35°E). The results show that there was an anomalous enhancement of electric field in F2-region close to the epicenter with maximal amplitude ∼2 mV/m (about 10 times of the background) at 15:00 LT on 9 May, which is in line with the amplitudes of anomalous electric field related to some previous earthquakes observed by satellites. 相似文献
632.
A coupled supersonic inlet-fan Navier–Stokes simulation method was developed by using COMSOL-CFD code. The flow turning, pressure rise and loss effects across blade rows of the fan and the inlet-fan interactions were taken into account as source terms of the governing equations without a blade geometry by a body force model. In this model, viscous effects in blade passages can also be calculated directly, which include the exchange of momentum between fluids and detailed viscous flow close to walls. NASA Rotor 37 compressor test rig was used to validate the ability of the body force model to estimate the real performance of blade rows. Calculated pressure ratio characteristics and the distribution of the total pressure, total temperature, and swirl angle in the span direction agreed well with experimental and numerical data. It is shown that the body force model is a promising approach for predicting the flow field of the turbomachinery. Then, coupled axisymmetric mixed compression supersonic inlet-fan simulations were conducted at Mach number 2.8 operating conditions. The analysis includes coupled steady-state performance, and effects of the fan on the inlet. The results indicate that the coupled simulation method is capable of simulating behavior of the supersonic inlet-fan system. 相似文献
633.
This paper conducts a simulation study of a novel aircraft environmental control system based on membrane dehumidification(MD-ECS),and compares the system with the up-to-date four-wheel high pressure de-water system(4WHPDW-ECS).Mathematical models for the two systems are established,and a system simulation using a numerical technique is performed to analyze and compare the cooling performance of the two systems.Simulation results show that the cooling capacity of MD-ECS is much higher than that of 4WHPDW-ECS under the same working conditions,indicating that the novel system is theoretically feasible and promising.The effects of the sweep ratio of the membrane dehumidifier on the dehumidification and cooling performance of the system is also investigated. 相似文献
634.
635.
利用OpenGL显示叶轮造型及模拟加工 总被引:1,自引:0,他引:1
分析了OpenGL编程原理以及OpenGL与Windows图形设备接口GDI之间的关系,介绍了OpenGL进行叶轮造型显示及虚拟加工的应用方法. 相似文献
636.
在分析研究直升机桨叶耐颗粒物/砂磨蚀标准主要技术要素的基础上,全面对比分析了MIL-STD-3033、ГОСТР52560-2006、GJB 1171-1991等国内外标准的基本内容,提出了装备研制及标准化工作相关建议。 相似文献
637.
An experimental method and a theoretical analysis based on continuum damage mechan-ics are applied for the defects tolerance of fixed plate. The defects type studied in this article is scratch, which i... 相似文献
638.
639.
低成本IMU/GPS组合导航系统研究 总被引:2,自引:0,他引:2
GPS/INS组合导航系统已在一定领域得到应用,而INS昂贵的价格限制了它的广泛应用,本文采用低成本惯性测量组件(IMU)设计了低成本IMU/GPS组合系统的硬件和相应的软件,进行了静态实验和数据处理,系统的俯仰角和横滚角误差均小于0.2°,实验结果表明,低成本组合系统的性能较好,而其性能价格比更高。 相似文献
640.
提出通过模型参数的模糊比例积分自适应调节,以校正基于模型的飞控系统故障检测中的系统数学模型偏差。针对模型中误差差较大的迎角导数值,将俯仰角加速度的测量值与教学模型估计值之差作为比例积分调节的反馈量,动态实时校正数学模型参数。 相似文献