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CFD Simulation of Kerosene-Fueled Supersonic Combustion Ramjet Combustor Experiments
Wan T(万田); Chen LH(陈立红); Wang J(王晶); Fan XJ(范学军); Zhang XY(张新宇); Wan, TA (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam LHD, Beijing 100190, Peoples R China.
会议录名称PROCEEDINGS OF 2010 ASIA-PACIFIC INTERNATIONAL SYMPOSIUM ON AEROSPACE TECHNOLOGY, VOL 1 AND 2
2010
会议名称Asia-Pacific International Symposium on Aerospace Technology
会议日期SEP 13-15, 2010
会议地点Xian, PEOPLES R CHINA
摘要The kerosene-fueled scramjet combustor experiments are numerically simulated, for the purpose of code validation and better understanding of flow structure. Full chemically reacting Navier-Stokes equation is numerically solved, and a global reaction mechanism and a reduced 12 species 12 step reaction mechanism are used for kerosene combustion. Computational results using different level of grid refinement and wall boundary conditions are compared with the experimentally measured data. In addition, computed results with different reaction mechanisms are compared. The computed and experimental results agree well. Three dimensional flow structures of different fuel injection scheme are compared. The results show that the subsonic region of the in-cavity fuel injection is located near the sidewall, whereas for the case with upstream single-hole fuel injection, the subsonic region is located near the symmetry plane.
WOS记录号WOS:000288362800275
ISBN号978-7-5612-2899-9
收录类别CPCI-S ; EI
语种英语
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文献类型会议论文
条目标识符http://dspace.imech.ac.cn/handle/311007/58875
专题高温气体动力学国家重点实验室
通讯作者Wan, TA (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam LHD, Beijing 100190, Peoples R China.
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Wan T,Chen LH,Wang J,et al. CFD Simulation of Kerosene-Fueled Supersonic Combustion Ramjet Combustor Experiments[C]PROCEEDINGS OF 2010 ASIA-PACIFIC INTERNATIONAL SYMPOSIUM ON AEROSPACE TECHNOLOGY, VOL 1 AND 2,2010.
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