中国科学院机构知识库网格系统: 检索

Conceptual design and heat transfer performance of a flat-tile water-cooled divertor target 期刊论文 OAI收割
PLASMA SCIENCE & TECHNOLOGY, 2021, 卷号: 23
作者: LI, Lei; Han, Le; Zi, Pengfei; Cao, Lei; Xu, Tiejun

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收藏 | 浏览/下载：46/0 | 提交时间：2021/08/30

CFETR heat transfer performance parametric design and optimization HHF tests flat-tile divertor target

Modelling the scores and performance statistics of NBA basketball games 期刊论文 OAI收割
COMMUNICATIONS IN STATISTICS-SIMULATION AND COMPUTATION, 2020, 卷号: 49, 期号: 10, 页码: 2604-2616
作者: Song, Kai; Zou, Qingrong; Shi, Jian

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收藏 | 浏览/下载：31/0 | 提交时间：2021/01/14

NBA outcome forecast Bivariate normal mean regression Performance statistics Betting strategy Market efficiency tests

Performance of the insulation mock-ups for the ITER PF6 coil 期刊论文 OAI收割
FUSION ENGINEERING AND DESIGN, 2018, 卷号: 137, 期号: 无, 页码: 362-372
作者: Wu, Huan; Song, Yuntao; Lu, Kun; Wei, Jing; Shen, Guang

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收藏 | 浏览/下载：35/0 | 提交时间：2020/03/31

Performance Electrical and mechanical Tests Insulation Mock-ups ITER PF6 coil

Development of fast response freezing valve for liquid lithium application in tokamak 期刊论文 OAI收割
VACUUM, 2016, 卷号: 127, 期号: 无, 页码: 73-81
作者: Chen, Zhaoxi; Yang, Qingxi; Song, Yuntao; Hu, Jiansheng; Zuo, Guizhong

收藏 | 浏览/下载：39/0 | 提交时间：2017/07/19

Fusion Liquid Lithium Freezing Valve Performance Tests

爆轰驱动膨胀管性能研究 期刊论文 OAI收割
航空学报, 2016, 卷号: 37, 期号: 3, 页码: 810-816
作者: 周凯; 汪球; 胡宗民; 姜宗林

收藏 | 浏览/下载：33/0 | 提交时间：2016/12/16

hypervelocity detonation-driven expansion tube performance study experimental tests numerical simulation

Investigation of pipe separation technology in the oilfield 会议论文 OAI收割
2nd International Conference on Energy, Environment and Sustainable Development, EESD 2012, Jilin, PEOPLES R CHINA, OCT 12-14, 2012
作者: Zhong XF(钟兴福); Wu YX(吴应湘); Li SM; Wei PJ

收藏 | 浏览/下载：29/0 | 提交时间：2013/02/26

Crude oil Oil fields Phase separation Planning Sustainable development Compact separators Gravity separator Low costs Mixture flow Oil-water-gas Performance tests Separation technologies Technological process

Aerodynamic design on China new high-speed trains 会议论文 OAI收割
1st International Workshop on High-Speed and Intercity Railways, IWHIR 2011, Shenzhen, Hong Kong, China, JULY 19-22, 2011
作者: Yang GW(杨国伟); Yang GW(杨国伟)

收藏 | 浏览/下载：35/0 | 提交时间：2013/02/06

Railroad cars Railroad transportation Railroad tunnels Railroads Wind effects Aerodynamic designs Aerodynamic noise Aerodynamic performance Cross-wind effects High speed trains Pressure waves Running conditions Running tests Running-in Wind tunnel experiment

Modular aircraft simulation platform based on simulink (EI CONFERENCE) 会议论文 OAI收割
2010 IEEE International Conference on Mechatronics and Automation, ICMA 2010, August 4, 2010 - August 7, 2010, Xi'an, China
Chen C.-Q.; Ji Y.

收藏 | 浏览/下载：28/0 | 提交时间：2013/03/25

Aircraft simulation platform is the most important supporting technology in the aircraft development process. This simulation platform can be used for validating the design of subsystem and also it provides the necessary data for the Aircraft design. Wind has great impact on the flight parameter. In order to accurately simulate the wind model and calculate the flight parameters a simulation modeling method for flight parameter simulation platform under wind field environment is established. Firstly the various sub-systems which affecting flight parameters are analyzed some mathematical models of the flight parameter simulation platform is established. Secondly the atmospheric wind field is studied to analyze the impact on its trajectory. Then the model is built in the Simulink toolbox in the Matlab which is based on the principles of hierarchy and modularity using C MEX S-function for the complex kinetic equations. Finally when the models have been established encapsulating models for several subsystem and assembling them for the Aircraft simulation platform based on the unified interface. The simulation tests (including the performance test of a certain gliding Aircraft the wind influence test of a certain uncontrolled aircraft) prove the simulation capability of the platform and its calculating step can reach 1 ms. Comparing simulation with field test data of a certain uncontrolled aircraft it shows that the relative deviation of range is 0.47% the relative deviation of maximal altitude is 2.1%. Taking relevant standards as a reference standard it is demonstrated the platform is reliable meets the engineering accuracy requirements. 2010 IEEE.

Flaking and degradation of polyurethane coatings after 2 years of outdoor exposure in Lhasa 期刊论文 OAI收割
Chinese Science Bulletin, 2010, 卷号: 55, 期号: 7, 页码: 650-655
F. C. Liu; Y. S. Hao; Z. Y. Wang; H. W. Shi; E. H. Han; W. Ke

收藏 | 浏览/下载：20/0 | 提交时间：2012/04/13

FTIR XPS AFM degradation weathering flake urethane Lhasa weathering resistance performance tests films xps

Design and DSP implementation of star image acquisition and Star point fast acquiring tracking (EI CONFERENCE) 会议论文 OAI收割
2nd International Symposium on Advanced Optical Manufacturing and Testing Technologies: Optical Test and Measurement Technology and Equipment, November 2, 2005 - November 5, 2005, Zian, China
作者: Wang X.; Wang X.; Wang X.

收藏 | 浏览/下载：22/0 | 提交时间：2013/03/25

Star sensor is a special high accuracy photoelectric sensor. Attitude acquisition time is an important function index of star sensor. In this paper the design target is to acquire 10 samples per second dynamic performance. On the basis of analyzing CCD signals timing and star image processing a new design and a special parallel architecture for improving star image processing are presented in this paper. In the design the operation moving the data in expanded windows including the star to the on-chip memory of DSP is arranged in the invalid period of CCD frame signal. During the CCD saving the star image to memory DSP processes the data in the on-chip memory. This parallelism greatly improves the efficiency of processing. The scheme proposed here results in enormous savings of memory normally required. In the scheme DSP HOLD mode and CPLD technology are used to make a shared memory between CCD and DSP. The efficiency of processing is discussed in numerical tests. Only in 3.5ms is acquired the five lightest stars in the star acquisition stage. In 43us the data in five expanded windows including stars are moved into the internal memory of DSP and in 1.6ms five star coordinates are achieved in the star tracking stage.