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《JOURNAL OF SHANGHAI JIAOTONG UNIVERSITY》 1998-01
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Numerical Simulation of ShockWave/BoundaryLayer Interaction Problems

Dong Wei Fan Xuji(Department of Power Machinery Engineering, Shanghai Jiaotong University)  
An efficient finite volume scheme is presented for solving shockwave/boundarylayer interaction problem. This scheme has been applied to analyze the shockwave/boundarylayer interaction problems and their effects on pressure and heating rates. Some of the computed results are compared with the available wind tunnel data.
【CateGory Index】: V47
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【Co-references】
Chinese Journal Full-text Database 10 Hits
1 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
2 Kang Honglin Yan Chao Li Tinghe(School of Aeronautic Science and Technology,Beijing University of Aeronautics and Astronautics,Beijing 100083,China)Guo Dilong(Institute of Mechanics,Chinese Academy of Sciences,Beijing 100080,China);Numerical study of aeroheating predictions for hypersonic reentry bodies[J];Journal of Beijing University of Aeronautics and Astronautics;2006-12
3 Wu Songping Lu Ye Zheng Bo (Beijing University of Aeronautics and Astronautics,Dept. of Flight Vehicle Design and Applied Mechanics);Implicit Schemes for Numerical Simulations of Hypersonic Nonequilibrium Flows[J];Journal of Beijing University of Aeronautics and Astronautics;1998-06
4 Zhang Xiaoying1,Zhu Dingqiang2,Xiang Hongjun2,Cai Guobiao2(South China University of China,Guangzhou,510640;Beijing University of Aeronautics and Astronautics,Beijing,100083);Quasi-three Dimensional Calculation of Missile Wall Temperature and Infrared Radiation of the Missile[J];Missiles and Space Vehicles;2006-04
5 ZHU Yun-ji, SHI Zhong-ke (College of Automation, Northwestern Polytechnical University, Xi'an 710072, China);Several Problems of Flight Characteristics and Flight Control for Hypersonic Vehicles[J];Flight Dynamics;2005-03
6 JIN Ling WANG An-Ling GUI Ye-Wei GENG Xiang-Ren TANG Wei (China Aerodynamics Research and Development Center,Mianyang 621000,China);THE RESEARCH OF THE THERMAL CORRIDOR OF THE X43[J];Journal of Engineering Thermophysics;2007-02
7 ;Development Trend of High-Supersonic Vehicle[J];International Aviation;1998-03
8 YUE Faren1, YANG Jun1, JIANG Guiqing2, LU Rui1//1. The 41st Institute of the Fourth Academy of CASC, Xi'an 710025, China;2. The 701st Institute of CASC, Beijing 100074,China.;Aerodynamic heating calculation of micro-gravity rocket[J];Journal of Solid Rocket Technology;2003-01
9 SHAN Yong,ZHANG Jing-zhou,GUO Rong-wei(College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China);Numerical computation and analysis of the infrared radiation characteristic of missile scarfskin[J];Journal of Aerospace Power;2008-02
10 JIANG You-di,DONG Wei,CHEN Yong(School of Mechanical Engineering,Shanghai Jiao Tong University,Shanghai 200240,China);Surface heat flux calculation of variable entropy flow for hypersonic blunt bodies[J];Journal of Aerospace Power;2008-09
【Secondary References】
Chinese Journal Full-text Database 5 Hits
1 Yang Kai1,Gao Xiaowei2(1.Department of Engineering Mechanics,Southeast University,Nanjing,210096;2.Department of Aeronautics and Astronautics,Dalian University of technology,Dalian,116024);Engineering Algorithm for Aeroheating Environment of Hypersonic Aircrafts[J];Missiles and Space Vehicles;2010-04
2 CHENG Xing-hua,YANG Tao,CHANG Zhong-dong (College of Aerospace and Material Engineering, National University of Defense Technology,Changsha 410073,China);Influence of entropy layer on aerodynamics parameters for hypersonic 2-D blunt wedge[J];Journal of Aerospace Power;2012-06
3 YANG Kai*1,GAO Xiao-wei2(1.Department of Engineering Mechanics,Southeast University,Nanjing 210096,China;2.State Key Laboratory of Structural Analysis for Industrial Equipment,Dalian University of Technology,Dalian 116024,China);Computation of aero-heating environment for key places of hypersonic aircrafts[J];Chinese Journal of Computational Mechanics;2012-01
4 Wu Dan,Xu Changyue,Sun Jianhong(College of Aerospace Engineering,Nanjing University of Aeronautics & Astronautics,Nanjing,210016,China);Numerical Simulation About Effect of Mach Number on Aerodynamic Heating Around Cabin[J];Journal of Nanjing University of Aeronautics & Astronautics;2011-04
5 XUE Peng-fei,GONG Chun-lin,GU Liang-xian(College of Astronautics,Northwestern Polytechnical University,Xi'an Shanxi 710072,China);Study of Method for Aerothermal Heating Calculating Based on Axisymmetric Analogue[J];Computer Simulation;2012-06
China Proceedings of conference Full-text Database 1 Hits
1 JI Kexing SONG Hongwei HUANG Chenguang (Hypersonic Research Center CAS, No.15 Beisihuanxi Road, Beijing 100190, China) (Key Laboratory of Hydrodynamic and Ocean Engineering, Institute of Mechanics, CAS, No.15 Beisihuanxi Road, Beijing 100190, China);INFLUENCE OF TRANSIENT TEMPERATURE AND THERMAL STRESS ON THE VIBRATION MODE OF ACTIVE COOLING SCRAMJET[A];[C];2010
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