Full-Text Search:
Home|Journal Papers|About CNKI|User Service|FAQ|Contact Us|中文
《Acta Aerodynamica Sinica》 2002-S1
Add to Favorite Get Latest Update

Parallel computation for low mach number flows

XIANG Da ping, DENG Xiao gang, MAO Mei liang (China Aerodynamics Research and Development Center, Mianyang 621000,China)  
In this paper, we carried out parallel computation study of a new method for low Mach number flows developed by Deng etc. A new algorithm for interface and real boundary treatment has been designed for grid blocks with different topology, and a general parallel computation code have been developed. Running on a massive parallel processing (MPP) machine, this code obtained a good speed-up ratio. Parallel computing results for low Reynolds number flows around spheroid and high Reynolds number flow around 6:1 prolate spheroid agree well with serial results.
【Fund】: 国防科学技术预先研究基金资助项目;; 国有自然科学基金 (86 3- 30 6主题 )资助项目
【CateGory Index】: V211.3
Download(CAJ format) Download(PDF format)
CAJViewer7.0 supports all the CNKI file formats; AdobeReader only supports the PDF format.
Chinese Journal Full-text Database 10 Hits
1 Bing Wang · Xue-Ying Deng · Bao-Feng Ma · Zhen Rong Key Laboratory of Fluid Mechanics,(Beihang University),Ministry of Education,Beihang University,Beijing 100191,China;Effects of tip perturbation and wing locations on rolling oscillation induced by forebody vortices[J];力学学报(英文版);2010-05
2 Fan Xiaoqiang Li Hua Ding Meng (College of Aerospace and Material Science, National University of Defence Technology, Changsha, 410073);PREDICTED HEATING DISTRIBUTIONS FOR BLUNT BICONIC AT AN ANGLE OF ATTACK[J];Acta Armamentarii;2002-01
3 Zhan Jingxia Wang Jinjun Li Yachen (Fluid Mechanics Institute, Beijing University of Aeronautics and Astronautics, 100083);EXPERIMENTAL INVESTIGATION OF GURNEY FLAPS ON THE AERODYNAMIC CHARACTERISTICS OF HIGHLY SWEPT-BACK PLANE-DELTA WING[J];Acta Armamentarii;2004-03
4 L Xiao bin ZHU Zi qiang (Beijing University of Aeronautics and Astronautics,Dept. of Flight Vehicle Design and Applied Mechanics);2D Multiblock and Parallel Method to Solve Transonic Euler Equations[J];JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS;2000-02
5 Li Junzhe Yan Chao Ke Lun Zhang Shuting (School of Aeronautics Science and Technology, Beijing University of Aeronautics and Astronautics, Beijing 100083, China);Research on scheme effect of computational fluid dynamics in aerothermal[J];Journal of Beijing University of Aeronautics and Astronautics;2003-11
6 Ma Hui Zhao Lie Wang Famin (Institute of Mechanics, Chinese Academy of Sciences, Beijing 100080, China);Numerical simulations of hypersonic three-dimensional chemical non-equilibrium flows[J];Journal of Beijing University of Aeronautics and Astronautics;2004-02
7 Ma Hui\ Wang Famin(Institute of Mechanics, Chinese Academy of Sciences, Beijing 100080, China);Calculation method of source terms in high temperature chemical nonequilibrium flows[J];Journal of Beijing University of Aeronautics and Astronautics;2004-07
8 Yan Chao Xie Lei Li Yunxiao(Beijing University of Aeronautics and Astronautics,Dept. of Flight Vehicle Design and Applied Mechanics)[WT〗;Optimization Aerodynamic Design for Transonic Airfoil[J];JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS;1998-03
9 WANG Ying QU Yi xin (College of Chemical Engineering, Beijing University of Chemical Technology, Beijing 100029,China);Cluster of PC and its development environment LINUX OS and MPI and application[J];JOURNAL OF BEIJING UNIVERSITY OF CHEMICAL TECHNOLOGY;2001-04
10 ZHU Xun, XIN Ming-dao (Institute of Engineering Thermophysics,Chongqing University,Chongqing 400044,China);Analysis for Heat Transfer in Micro-annular Channel with Unsymmetrically Heated Walls in Slip Flow Regime[J];Journal of Chongqing University(Natural Science Edition);2001-03
【Secondary References】
Chinese Journal Full-text Database 10 Hits
1 Zheng Wenwu,Li Xianxu,Huang Zhiqin(Guangdong Research Institute of China Telecom Co.,Ltd.,Guangzhou 510630,China);Technolical Analysis of Parallel Computing in Cloud Computing[J];Telecommunications Science;2011-12
2 LOU Ben-zhuo(Shanxi University of Technology,Hanzhong Shanxi 723003,China);The Research on Optimization for Heat Treatment Parameters of Grade E Steel[J];Heat Treatment Technology and Equipment;2008-06
3 Li Shengmei1,Cheng buqi2,Gao Xingyu3,Qiao Lin1,and Tang Zhizhong11(Department of Computer Science and Technology,Tsinghua University,Beijing 100084)2(Programming Systems Laboratory,Intel China Research Center,Beijing 100080)3(Academy of Mathematics and Systems Science,Chinese Academy of Sciences,Beijing 100190);Principal Component Linear Regression Analysis on Performance of Applications[J];Journal of Computer Research and Development;2009-11
4 LU Ping-jing,CHE Yong-gang,WANG Zheng-hua (School of Computer Science,National University of Defense Technology,Changsha 410073,China);Memory Hierarchy Optimization Based on Empirical Search[J];Computer Engineering and Applications;2006-34
5 SHAN Ying,WU Jian-ping,WANG Zheng-hua(College of Computer Science,National University of Defence Technology,Changsha Hunan 410073,China);Hierarchical Parallel Programming Model and Parallelization and Optimization Techniques Based on SMP Cluster[J];Application Research of Computers;2006-10
6 YU Gang, LI Dong(Northwestern Polytechnical University ,Xi'an 710072 ,P.R.China);Optimization Design of Airfoil Based on Hybrid Genetic Algorithm and Compound Form Method[J];Science Technology and Engineering;2007-10
7 AO Fu-jiang DU Jing MA Xiao-zun WANG Lian-dong(Unit 63880 of PLA,Luoyang 471003,China);Research on the Applicability between Program and Platform in High Performance Simulation[J];Computer Science;2012-S1
8 PAN Sha,LI Hua,XIA Zhi-xun(School of Aerospace and Material Engineering, National University of Defense Technology,Changsha 410073,China);High-Performance Parallel Computation Application for Aerospace CFD Numerical Simulation[J];Computer Engineering & Science;2012-08
9 Tian Xiaohu,Zhang Binqian,Shen Dong(School of Aeronautics,Northwestern Polytechnical University,Xi′an 710072);Hybrid Optimization Method Based on the Best Vertex and Its Application to Optimization Design of Airfoil[J];Mechanical Science and Technology for Aerospace Engineering;2012-12
10 GONG Chun-ye;BAO Wei-min;TANG Guo-jian;WANG Ling;SUN Xue-gong;LIU Jie;Laboratory of Science and Technology on Space Physics;College of Aerospace Science and Technology,National University of Defense Technology;College of Computer Science,National University of Defense Technology;;Recent progress in high-performance parallel computing of the aerospace area[J];Computer Engineering & Science;2014-09
©2006 Tsinghua Tongfang Knowledge Network Technology Co., Ltd.(Beijing)(TTKN) All rights reserved