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浏览/检索结果: 共14条,第1-10条 帮助

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A gas-surface interaction algorithm for discrete velocity methods in predicting rarefied and multi-scale flows: For Maxwell boundary model 期刊论文  OAI收割
COMPUTERS & MATHEMATICS WITH APPLICATIONS, 2024, 卷号: 175, 页码: 570-601
作者:  
Chen, Jianfeng;  Liu, Sha;  Wang Y(王勇);  Zhuo, Congshan;  Yang, Yanguang
  |  收藏  |  浏览/下载:2/0  |  提交时间:2024/12/02
A Modified Symmetric and Antisymmetric Decomposition-Based Three-Dimensional Numerical Manifold Method for Finite Elastic-Plastic Deformations 期刊论文  OAI收割
ACTA MECHANICA SOLIDA SINICA, 2020, 卷号: 33, 期号: 1, 页码: 71-97
作者:  
Ke, Jinfu
  |  收藏  |  浏览/下载:16/0  |  提交时间:2021/05/25
Unified Overload Method of Slope Stability Analysis Based on Potential Sliding Direction 期刊论文  OAI收割
KSCE JOURNAL OF CIVIL ENGINEERING, 2018, 卷号: 22, 期号: 9, 页码: 3254-3262
作者:  
Xue, Haibin;  Dang, Faning;  Yin, Xiaotao;  Ding, Weihua
  |  收藏  |  浏览/下载:24/0  |  提交时间:2020/04/08
Analyzing the general biased data by additive risk model 期刊论文  OAI收割
SCIENCE CHINA-MATHEMATICS, 2017, 卷号: 60, 期号: 4, 页码: 685-700
作者:  
Li YanFeng;  Ma HuiJuan;  Wang DeHui;  Zhou Yong
  |  收藏  |  浏览/下载:27/0  |  提交时间:2018/07/30
Efficient parallel implementation of the lattice Boltzmann method on large clusters of graphic processing units 期刊论文  OAI收割
CHINESE SCIENCE BULLETIN, 2012, 卷号: 57, 期号: 7, 页码: 707-715
作者:  
Xiong QinGang;  Li Bo;  Xu Ji;  Fang XiaoJian;  Wang XiaoWei
收藏  |  浏览/下载:39/0  |  提交时间:2013/10/26
Precision detection of CCD splicing based on template matching algorithm (EI CONFERENCE) 会议论文  OAI收割
IEEE 2nd International Conference on Computing, Control and Industrial Engineering, CCIE 2011, August 20, 2011 - August 21, 2011, Wuhan, China
作者:  
Zhang X.;  Zhang X.;  Yang L.;  Zhang X.;  Yang L.
收藏  |  浏览/下载:32/0  |  提交时间:2013/03/25
The remote sensing camera in large field and wide cover needs CCD with enough pixels. But the existing CCD cannot satisfy the practical needs. Therefore several pieces of CCD which has insufficient pixels are spliced to get a long CCD array with plenty of pixels. The precision requirements of CCD splicing are very strict  so that the same high accuracies are required in the precision detection of CCD splicing. When detecting precision of CCD splicing  the graphical markers with simple geometric structure in the CCD package are selected as templates. The position precision data of the graphical markers in each CCD are obtained using the template matching algorithm. Using the unified objective templates  the focal plane which has multi-chip of CCD is detected by template matching algorithm. Experiment results show that the template matching algorithm can enhance the located precision of each CCD to 0.347m. The splicing precision detection with template matching algorithm can avoid the subjective error caused by the conventional detection method. And its results are more accurate. In addition  without manual intervention in the process of precision detection  the efficiency of precision detection is improved. 2011 IEEE.  
An Adaptive Multimoment Global Model on a Cubed Sphere 期刊论文  OAI收割
Monthly Weather Review, 2011, 卷号: 139, 期号: 2, 页码: 523-548
作者:  
Chen CG(陈春刚);  Xiao F(肖锋);  Li XL
收藏  |  浏览/下载:30/0  |  提交时间:2012/04/01
The theory of nonlinear interfacial-internal wave propagation in three-layer fluid systems 期刊论文  OAI收割
ACTA PHYSICA SINICA, 2010, 卷号: 59, 期号: 10, 页码: 7149-7157
作者:  
Wen Wen-Ying;  Chen Xiao-Gang;  Song Jin-Bao
收藏  |  浏览/下载:22/0  |  提交时间:2015/07/20
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:26/0  |  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.  
A local feature based simplification method for animated mesh sequence (EI CONFERENCE) 会议论文  OAI收割
2010 2nd International Conference on Computer Engineering and Technology, ICCET 2010, April 16, 2010 - April 18, 2010, Chengdu, China
作者:  
Wang B.;  Wang B.;  Zhao J.;  Zhang S.
收藏  |  浏览/下载:23/0  |  提交时间:2013/03/25
Although animated meshes are frequently used in numerous domains  only few works have been proposed until now for simplifying such data. In this paper  we propose a new method for generating progressive animated models based on local feature analysis and deformation area preservation. We propose the use of solid angle and height value for a non-hyperbolic vertex to define the local feature parameter. This local factor is embedded to the vertex quadric error matrix when calculating the edge collapse cost. In order to preserve the areas with large deformation  we add deformation degree weight to the aggregated quadric errors when computing the unified edge contraction sequence. Finally  a mesh optimization process is proposed to further reduce the geometric distortion for each frame. Our approach is fast  easy to implement  and as a result good quality dynamic approximations with well-preserved fine details can be generated at any given frame. 2010 IEEE.