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An improved stiff-ODE solving framework for reacting flow simulations with detailed chemistry in OpenFOAM 期刊论文
COMBUSTION THEORY AND MODELLING, 2023, 卷号: 27, 期号: 1, 页码: 57-82
作者:  Wu K(吴坤);  Jiang, Yuting;  Huo ZJ(霍志杰);  Cheng D(程迪);  Fan XJ(范学军)
收藏  |  浏览/下载：15/0  |  提交时间：2023/02/03
Dynamic profiles of tar products during Naomaohu coal pyrolysis revealed by large-scale reactive molecular dynamic simulation 期刊论文
FUEL, 2019, 卷号: 253, 页码: 910-920
作者:  Zheng, Mo;  Li, Xiaoxia;  Wang, Meijun;  Guo, Li
收藏  |  浏览/下载：57/0  |  提交时间：2019/09/03
Toward high-efficiency and detailed Monte Carlo simulation study of the granular flow spallation target 期刊论文
NUCLEAR INSTRUMENTS & METHODS IN PHYSICS RESEARCH SECTION A-ACCELERATORS SPECTROMETERS DETECTORS AND ASSOCIATED EQUIPMENT, 2018, 卷号: 882, 页码: 117-123
作者:  Zhang, Xun-Chao;  Cai, Han-Jie;  Zhang, Zhi-Lei;  Fu, Fen;  Li, Jian-Yang
收藏  |  浏览/下载：22/0  |  提交时间：2018/05/31
Dynamic modelling of the VSC-HVDC for analytical studies 会议论文
作者:  Song, Guobing;  Wang, Ting;  Huang, Xinghua;  Gu, Yaobin;  Liu, Yakun
收藏  |  浏览/下载：16/0  |  提交时间：2019/11/26
Fixed topology Thevenin equivalent fully detailed model for nonlinear capacitances 期刊论文
ELECTRONICS LETTERS, 2017, 卷号: 53, 页码: 42-43
作者:  Zhang, Feng;  Wang, Kangping;  Yang, Xu;  Cheng, Shi
收藏  |  浏览/下载：13/0  |  提交时间：2019/11/26
Large eddy simulation of spray and combustion characteristics with realistic chemistry and high-order numerical scheme under diesel engine-like conditions 期刊论文
ENERGY CONVERSION AND MANAGEMENT, 2015, 卷号: 93, 页码: 377-387
作者:  Zhou, Lei;  Luo, Kai Hong;  Qin, Wenjin;  Jia, Ming;  Shuai, Shi Jin
收藏  |  浏览/下载：11/0  |  提交时间：2019/12/09
Aircraft flight simulation with landing gear based on multi-domain modeling technology (EI CONFERENCE) 会议论文
2012 2nd International Conference on Computer Application and System Modeling, ICCASM 2012, July 27, 2012 - July 29, 2012, Shenyang, China
Li M.; Hao X.; Han X.; Jia H.
收藏  |  浏览/下载：11/0  |  提交时间：2013/03/25
Establishment of airplane flight model and simulation analysis of landing behavior (EI CONFERENCE) 会议论文
2nd Annual Conference on Electrical and Control Engineering, ICECE 2011, September 16, 2011 - September 18, 2011, Yichang, China
Li M.; Li D.-W.; Jia H.-G.; Li L.
收藏  |  浏览/下载：17/0  |  提交时间：2013/03/25
This paper create a high fidelity plant model of an aircraft landing gear to inclusion into a full aircraft flight simulation for accurately analyzing the performance and influence of landing gear system. The use of domain specific modeling software enables detailed modeling of the physics and facilitates accurate computational simulation of the flight dynamic  aerodynamic  landing gear dynamic and mechanical loads that occur when the landing gear are deployed and retracted during landing and take-off operations. The parameter design space is easily searched by considering a number of different landing scenarios including touching down on one wheel first  to optimize the design. The simulation results show that the aircraft landing gear system mathematical model established appropriately reflects the change of force and moment in the process of taking off and landing  and it is actual in the physical process. 2011 IEEE.  
Aircraft landing gear simulation using multidomain modeling technology (EI CONFERENCE) 会议论文
2011 International Conference on Information Technology, Computer Engineering and Management Sciences, ICM 2011, September 24, 2011 - September 25, 2011, Nanjing, Jiangsu, China
Li M.; Hao X.-Y.; Han X.-F.; Jia H.-G.
收藏  |  浏览/下载：30/0  |  提交时间：2013/03/25
In order to accurately analyze the performance and influence of landing gear system  this paper presents a high fidelity plant model of an aircraft landing gear to inclusion into a full aircraft flight simulation. The use of domain specific modeling software enables detailed modeling of the physics and facilitates accurate computational simulation of the flight dynamic  aerodynamic  landing gear dynamic and mechanical loads that occur when the landing gear are deployed and retracted during landing and take-off operations. The parameter design space is easily searched by considering a number of different landing scenarios including touching down on one wheel first  to optimize the design. The simulation results show that the aircraft landing gear system mathematical model established appropriately reflects the change of force and moment in the process of taking off and landing  and it is improve the precision of flight simulation. 2011 IEEE.  
Analysis of measuring errors for the visible light phase-shifting point diffraction interferometer (EI CONFERENCE) 会议论文
2010 OSA-IEEE-COS Advances in Optoelectronics and Micro/Nano-Optics, AOM 2010, December 3, 2010 - December 6, 2010, Guangzhou, China
Zhang Y.; Jin C.; Lu Z.
收藏  |  浏览/下载：8/0  |  提交时间：2013/03/25
In order to improve the measuring accuracy of the visible light phase-shifting point diffraction interferometer (PS/PDI) for the extreme ultraviolet lithography (EUVL) aspheric mirrors  the main measuring errors will be discussed in this paper. At first  the elementary configuration and measuring principle of the visible light phase-shifting point diffraction interferometer are introduced briefly  then the different errors which are possible to affect the measuring result are summed up  the errors include PZT phase-shifting error  detector nonlinearity error  detector quantization error  wavelength instability error and intensity instability error of the laser source  vibration error  air refractivity instability error and so on. Through detailed analysis and simulation  the magnitude of these errors can be obtained. By analysing the reasons which cause these errors and the relationship between these errors and interferometer configuration parameters  some methods are put forward to avoid or restrain these errors accordingly.  

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