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Generalized wall function and its application to compressible turbulent boundary layer over a flat plate 会议论文
15th Asian Congress of Fluid Mechanics (15ACFM), Kuching, MALAYSIA, 2016-11-21
作者:  Liu, J.;  Wu, S. P.
收藏  |  浏览/下载：3/0  |  提交时间：2019/12/30
Implementation issues and benchmarking of lattice Boltzmann method for moving rigid particle simulations in a viscous flow 会议论文
Peng, Cheng; Teng, Yihua; Hwang, Brian; Guo, Zhaoli; Wang, Lian-Ping
收藏  |  浏览/下载：5/0  |  提交时间：2017/12/04
Slightly Rarefied Gas Flows Over a Sphere 会议论文
the 29th International Symposium on Rarefied Gas Dynamics, Xi'an, China, July 13-18, 2014
作者:  Cai CP;  Sun QH(孙泉华)
收藏  |  浏览/下载：20/0  |  提交时间：2015/01/01
Modeling of incompressible flow inside the involute channel 会议论文
Guilin, China, April 23, 2013 - April 24, 2013
作者:  Tao, Wen;  Li, Peng Bo
收藏  |  浏览/下载：16/0  |  提交时间：2020/11/15
A strong coupled CFD-CSD method on computational aeroelastity (EI CONFERENCE) 会议论文
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.  
Simulation of Wind Effects Embracing a Complex Shape Super High-Rise Steel TV Tower Using CFD 会议论文
ADVANCED MANUFACTURING SYSTEMS, PTS 1-3, 2011-04-09
作者:  Tan, Yaya[1];  Li, Chunxiang[2]
收藏  |  浏览/下载：8/0  |  提交时间：2019/04/30
Hydrodynamically numerical computation and efficiency correction on a supercritical pump with complex double-cases 会议论文
作者:  Yang, Congxin;  Wang, Xiuyong;  Cheng, Xiaorui;  Li, Yibin;  Zhang, Fengyu
收藏  |  浏览/下载：5/0  |  提交时间：2019/11/15
气体离心机二维供料射流的数值研究 会议论文
第五届北京核学会核技术应用学术交流会, CNKI
姜东君; 曾实; JIANG Dong-jun; ZENG Shi
收藏  |  浏览/下载：6/0
CFD Simulation of Kerosene-Fueled Supersonic Combustion Ramjet Combustor Experiments 会议论文
Asia-Pacific International Symposium on Aerospace Technology, Xian, PEOPLES R CHINA, SEP 13-15, 2010
作者:  Wan T(万田);  Chen LH(陈立红);  Wang J(王晶);  Fan XJ(范学军);  Zhang XY(张新宇)
收藏  |  浏览/下载：16/0  |  提交时间：2016/06/28
Hydrodynamically numerical computation on a supercritical pump with complex double-cases 会议论文
作者:  Yang, Congxin;  Wang, Xiuyong;  Cheng, Xiaorui;  Zhang, Fengyu
收藏  |  浏览/下载：7/0  |  提交时间：2019/11/15

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