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《JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS》 1997-03
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EFFECTS OF MIXED OUTFLOW BOUNDARY CONDITIONS FOR NUMERICAL SIMULATION OF VISCOUS JET FLOW

Chen Liang\ \ Yan Chao (Beijing University of Aeronautics and Astronautics,Dept. of Flight Vehicle Design and Applied Mechanics)  
A viscous jet flow from a hemisphere cylinder has been computed by numerical solution of three dimensional compressible N S equations using Jameson's finite volume method. The main purpose of this paper is to compare the effectiveness of treatment methods for mixed (subsonic freestream/supersonic jet flow) outflow boundary conditions,including: ①Riemann invariant method; ②extrapolation from the interiors; ③using the method 1 or 2 depending on the local Mach number; ④characteristic theory method.
【CateGory Index】: V211.3
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【References】
Chinese Journal Full-text Database 1 Hits
1 HUANG Xian-lu YAN Chao CHEN Liang LONG Yao-song (Beijing University of Aeronautics and Astronautics, Dept. of Flight Vehicle Design and Applied Mechanics);Numerical Analysis of Complex Flowfields Around Multi-Wing Missiles and Its Aerodynamic Force Computations[J];北京航空航天大学学报;2002-04
【Co-references】
Chinese Journal Full-text Database 2 Hits
1 Chen Liang\ \ Yan Chao (Beijing University of Aeronautics and Astronautics,Dept. of Flight Vehicle Design and Applied Mechanics);EFFECTS OF MIXED OUTFLOW BOUNDARY CONDITIONS FOR NUMERICAL SIMULATION OF VISCOUS JET FLOW[J];北京航空航天大学学报;1997-03
2 Yan Chao,Chen Liang (Institute of Fluid Dynamics,Beijing University of Aeronautics and Astronautics,Beijing,100083);NUMERICAL SIMULATION OF THREE DIMENSIONAL SEPARATED AND VORTICAL FLOW OVER HEMISPHERE CYLINDER[J];航空学报;1996-06
【Secondary References】
Chinese Journal Full-text Database 3 Hits
1 WANG Bo,LIN Yuan(The 92941st Unit of PLA,Huludao Liaoning 125001,China);The Jet Flow of the Vertical Launching System on Shipborne[J];海军航空工程学院学报;2012-01
2 ZHENG Qiu-ya1,4,YANG Zun-pao2,LIU Guo-jun3 (1.Science Institute,Xidian University,Xi'an,710071 China;2.Science Institute,Air Force Engineering University,Xi'an 710051;China;3.Aeronautical Laboratory of Computational Fluid Dynamics,Aeronautics Computing,Xi'an 710068,China;4.Science School of Changan University,Xi'an 710064,China);Aerodynamic Force Computations of Complex Flow-fields around Multi-Wing Air-Air Missiles[J];空军工程大学学报(自然科学版);2009-04
3 LIU Ji-min,SONG Gui-bao,MA Lin(Department of Airborne Vehicle Engineering,Navy Aeronautical Engineering Academy,Yantai 264001,China);Numerical Simulation of Three-Dimensional Flow Field about the Air-to-Surface Missile[J];航空计算技术;2006-05
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