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	An improved semi-implicit material point method for simulating large deformation problems in saturated geomaterials 期刊论文 OAI收割 COMPUTERS AND GEOTECHNICS, 2023, 卷号: 161, 页码: 17 作者: Yuan, Wei-Hai; Zheng, Houguo; Zheng, Xiangcou; Wang, Bin; Zhang, Wei \| 收藏 \| 浏览/下载：2/0 \| 提交时间：2025/06/27 Coupled problems Fractional step method Large deformation Material point method Porous media Stabilized technique
	Multi-exposure fusion based on illumination estimation for aerial cameras 期刊论文 OAI收割 Harbin Gongye Daxue Xuebao/Journal of Harbin Institute of Technology, 2018, 卷号: 50, 期号: 3, 页码: 90-96 作者: Shen, Xiaohe; Liu, Jinghong; Wang, Xuan \| 收藏 \| 浏览/下载：18/0 \| 提交时间：2019/09/17 Antennas Cameras Charge coupled devices Inverse problems Partial discharges Wavelet transforms
	A strong coupled CFD-CSD method on computational aeroelastity (EI CONFERENCE) 会议论文 OAI收割 2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011, July 15, 2011 - July 17, 2011, Inner Mongolia, China Xi R.; Jia H. 收藏 \| 浏览/下载：74/0 \| 提交时间：2013/03/25 In this paper a strong coupled CFD-CSD method is developed to simulate the aeroelastic phenomena. The CFD solver is based on the finite-volume algorithm for the Navier-Stokes equations on unstructured grid. The CSD solver solves the aeroelastic governing equations in the modal space. Their coupling is realized by a dual-time method. The spring-based smoothing method is adopted to deform and regenerate the aerodynamic grid. Two test cases are selected to validate the authors' method for static and dynamic aeroelastity .The results of the simulation for the static aeroelastic problems of a missile wing show that the Lift Coefficient and Drag Coefficient are severally 7% and 5% lower than those don't consider the elasticity of the wing. The results for the flutter boundary prediction of the AGARD 445.6 wing have been proved much closer to the experiment than using the DLM. This method can describe the effects of fluid viscosity more exactly for highly nonlinear transonic flight conditions. The calculation has proved reliable in the subsonic regime but not accurate enough in the supersonic regime. 2011 IEEE.
	Electromagnetic radiation test of power driver module in optical tracking system and electromagnetic compatibility (EI CONFERENCE) 会议论文 OAI收割 2010 International Conference on Computer, Mechatronics, Control and Electronic Engineering, CMCE 2010, August 24, 2010 - August 26, 2010, Changchun, China 作者: Yu H. 收藏 \| 浏览/下载：36/0 \| 提交时间：2013/03/25 In order to solve the conductive ring module's interference problems measured the electromagnetic radiation of Power drive module and used test results analysis the electromagnetic compatibility of the conductive ring identified and implemented appropriate EMC (electromagnetic compatibility) measures. When optical tracking system working test equipment can not be fixed. Therefore from the electromagnetic radiation theory the paper analyzed the electromagnetic radiation of the power drive module. From it determine the EMC pre-compliance test method for electromagnetic radiation of power drive module. Based on Test results calculate the interference voltage of wire in Conductive ring and then determine the corresponding EMC method. The results show that when The power drive module Radiate Electromagnetic waves wires would coupled common mode interference voltage its frequency is 3MHz amplitude is about 10V it would interfered the operation of sensor. By reducing the area of ground loops used shielded cables final rule out the interference. 2010 IEEE.