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《Journal of Beijing University of Aeronautics and Astronautics》 1998-06
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Numerical Simulation of Chemical Reacting Flow in H 2/O 2 Rocket Engine Thrust Chamber

Cai Guobiao (Beijing University of Aeronautics and Astronautics,School of Astronautics) Zhang Huazhao (Beijing Institute of Space System Engineering) Zhuang Fenggan (Beijing University of Aeronautics and Astronautics,Dept. of Flight Vehicle Design and Applied Mechanics)  
The viscous chemical reacting flow in the hydrogen oxygen rocket engine chamber and nozzle is simulated by using loosely coupled point implicit MacCormack scheme. In the numerical simulation the combustion process is modeled by using a 6 specis, 8 step finite rate chemical reaction model, and the Baldwin Lomax algebraic turbulent model is adopted. The distributions of flow parameters in the chamber and nozzle are presented. Analysis of the results show that the numerical simulation results are the same as the distributions of flow parameters in the hydrogen oxygen rocket engine chamber and nozzle, so the result is proved to be reliable. The work of this paper lays a foundation for the numerical simulation of two phase chemical reacting flow.
【Fund】: 国家自然科学基金
【CateGory Index】: V434.1
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【References】
Chinese Journal Full-text Database 4 Hits
1 Cai Guobiao (Beijing University of Aeronautics and Astronautics, School of Astronautics) Zhuang Fenggan (Beijing University of Aeronautics and Astronautics, Dept. of Flight Vehicle Design and Applied Mechanics);Direct Numerical Simulation on 2D H_2/O_2 Mixture and Flow[J];JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS;1999-06
2 Gao Yushan, Du Zhenggang, Jin Pin, Cai Guobiao (School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100191, China);Numerical simulation on the combustion characteristic of shear coaxial GO_2/ GCH_4 injector[J];Journal of Rocket Propulsion;2009-05
3 CAI Guobiao,MA Zhaokai,ZHANG Huazhao(1School of Astronautics, Beijing Univ. of Aeronautics and Astronautics, Beijing 100083,China;2Beijing Inst of Space System Engineering, Beijing 100076,China);Numerical simulation of C-H-O-N system liquid rocket engine nozzle flow[J];Journal of Propulsion Technology;2002-05
4 Cai Guobiao (School of Astronautics, Beijing University of Aeronautics and Astronautics·Beijing·100083)Zhang Huazhao (Beijing Institute of Space System Engineering·Beijing·100076)Zhuang Fenggan (China Aerospace Corporation·Beijing·100830);NUMERICAL SIMULATION ON CHEMICAL REACTING FLOW OF BIPROPELLANT ALTITUDE CONTROLLING THRUSTER NOZZLE[J];JOURNAL OF ASTRONAUTICS;2000-03
【Co-references】
Chinese Journal Full-text Database 10 Hits
1 Li Zongjie;Yu Kangyuan(College of Building Materials and Light Industry of BUU,Beijing,100054)(Beijing Meteorolgical College,Beijing,100081)[;The Continent Method for Nonequilibrium Flow of Chemical Reaction Inside Rocket Nozzle[J];JOURNAL OF BEIJING UNION UNIVERSITY;1995-01
2 Liu Jun Zeng Ming Qu Zhanghua (Department of Aerospace Technology, NUDT, Changsha, 410073);Numerical Simulation of 3 D Chemical Non equilibrium Flow over Reentry Capsule[J];JOURNAL OF NATIONAL UNIVERSITY OF DEFENSE TECHNOLOGY;1999-06
3 LIU Jun 1, ZHANG Han xin 2, GAO Shu chun 2 (1 College of Aerospace and Material Engineering, National Univ. of Defense Technology, Changsha 410073, China; 2 China Aerodynamics Research & Development Center, Mianyang 621000, China);A New Uncoupled Method for Numerical Simulation of Nonequilibrium flow[J];Journal of National University of Defense Technology;2000-05
4 WANG Ge,GU Xuan,HE Zheng(School of Civil Engineering, Harbin Engineering University,Harbin 150001,China);Numerical simulation of transient shock wave in a nozzle by PLM[J];Journal of Harbin Engineering University;2004-05
5 Sun Hongming (Shaanxi Power Machine Design and Research Institute, Xi’an 710100, China);Review of liquid oxygen/methane rocket engine[J];Journal of Rocket Propulsion;2006-02
6 DU Zheng-gang1,JIN Ping1,YANG Li-jun1,CAI Guo-biao1,ZHANG Meng-zheng2(1.School of Astronautics, Beijing University of Aeronautics and Astronautics,Beijing 100083,China;2.The 11th Research Institute of CASC,Xi'an 710100,China);Experimental investigation of flowrate characteristics of gas-gas injector[J];Journal of Aerospace Power;2007-03
7 WANG Xiao-wei,JIN Ping,DU Zheng-gang,CAI Guo-biao(School of Astronautics,Beijing University of Aeronautics and Astronautics,Beijing 100191,China);Simulation of cold flow and combustion characteristics of shear-coaxial GH_2/GO_2 injectors[J];Journal of Aerospace Power;2008-09
8 Zhou Weijiang, Wang Yiyun (Beijing Institute of Aerodynamics,Beijing,100074);NUMERICAL SIMULATION OF NON EQUILIBRIUM FLOW AROUND A BLUNT BODY[J];ACTA AERONAUTICA ET ASTRONAUTICA SINICA;1995-04
9 Huang Hua Qu Zhanghua (Department of Aerospace Technology, NUDT, Changsha 410073);Numerical Study for Symmetric Thermochemical NonequilibriumFlowfield with Eleven Species Air Model[J];ACTA AERODYNAMICA SINICA;1999-04
10 DONG Wei zhong, GAO Tie suo (China Aerodynamics Research and Development Center, Mianyang Sichuan 621000, China);Numerical studies of non-equilibrium flow-fields over acapsule-type hypersonic reentry vehicle[J];Acta Aerodynamica Sinica;2002-02
【Secondary References】
Chinese Journal Full-text Database 1 Hits
1 Cai guobiao 1 Guo Jingjing 1 Zhuang Fenggan 1 Zhu Xiaolan 2 (1 School of Astronautics,Beijing University of Aeronautics and Astronautics,Beijing 100083; 2 Lanzhou Institute of Physics,Lanzhou 73000);NUMERICAL SIMULATION OF VACUUM PLUME WITH CHEMICAL REACTION[J];Journal of Astronautics;2001-04
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