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浏览/检索结果: 共12条,第1-10条 帮助

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Aerodynamic optimization using passive control devices near the bogie cabin of high-speed trains 期刊论文  OAI收割
ACTA MECHANICA SINICA, 2022, 卷号: 38, 期号: 9, 页码: 16
作者:  
  |  收藏  |  浏览/下载:25/0  |  提交时间:2022/07/18
A study of the optimization design method for a high speed train 会议论文  OAI收割
Cagliari, Sardinia, Italy , 5-8 April 2016
作者:  
Zhao GL;  Sun ZX(孙振旭);  Yao SB(姚拴宝);  Guo DL(郭迪龙);  Yang GW(杨国伟)
  |  收藏  |  浏览/下载:31/0  |  提交时间:2018/11/08
Drag-reduction design on high-speed trains with intelligent optimization algorithm 会议论文  OAI收割
Ajaccio, Corsica, France, 8-11 April 2014
作者:  
Yang GW(杨国伟);  Yao SB(姚拴宝);  Guo DL(郭迪龙)
  |  收藏  |  浏览/下载:26/0  |  提交时间:2018/11/08
高速列车通过隧道时气动阻力特性的CFD仿真分析 期刊论文  OAI收割
中国铁道科学/CHINA RAILWAY SCIENCE, 2012, 卷号: 33, 期号: SUPPL.1, 页码: 33-38
作者:  
王一伟;  杨国伟;  黄晨光
收藏  |  浏览/下载:39/0  |  提交时间:2013/01/31
Three-dimensional aerodynamic optimization design of high-speed train nose based on GA-GRNN 期刊论文  OAI收割
Science China Technological Sciences, 2012, 期号: 5
作者:  
Yao SB(姚拴宝);  Guo DL(郭迪龙);  Yang GW(杨国伟)
收藏  |  浏览/下载:99/0  |  提交时间:2012/09/26
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:62/0  |  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.  
Estimating aerodynamic resistance of rough surfaces using angular reflectance 期刊论文  iSwitch采集
REMOTE SENSING OF ENVIRONMENT, 2010, 卷号: 114, 期号: 7, 页码: 1462-1470
作者:  
Chappell, Adrian;  Van Pelt, Scott;  Zobeck, Ted;  Dong, Zhibao
收藏  |  浏览/下载:27/0  |  提交时间:2019/10/08
Equivalent lenses of supersonic seeker's outflow refractive index field obtained by simulation and experiment (EI CONFERENCE) 会议论文  OAI收割
2008 International Conference on Optical Instruments and Technology: Optical Systems and Optoelectronic Instruments, November 16, 2008 - November 19, 2008, Beijing, China
Qun W.; Hongguang J.; Ming X.
收藏  |  浏览/下载:18/0  |  提交时间:2013/03/25
Aerodynamic characteristics research on wide-speed range waverider configuration 期刊论文  OAI收割
Science in China Series E-Technological Sciences, 2009, 卷号: 52, 期号: 10, 页码: 2903-2910
作者:  
Wang FM(王发民);  Ding HH(丁海河);  Lei MF(雷麦芳);  Wang FM;  Wang FM
收藏  |  浏览/下载:876/195  |  提交时间:2009/08/03
Improvement of an Aerodynamic Roughness Model With Meteorological Measurements and TM Image 会议论文  OAI收割
Zhou Y. L.; Sun X. M.; Ju W. M.
收藏  |  浏览/下载:14/0  |  提交时间:2012/06/30