| 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.
| |
| Source Publication | PROCEEDINGS OF 2010 ASIA-PACIFIC INTERNATIONAL SYMPOSIUM ON AEROSPACE TECHNOLOGY, VOL 1 AND 2 |
| 2010 | |
| Conference Name | Asia-Pacific International Symposium on Aerospace Technology |
| Conference Date | SEP 13-15, 2010 |
| Conference Place | Xian, PEOPLES R CHINA |
| Abstract | 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 ID | WOS:000288362800275 |
| ISBN | 978-7-5612-2899-9 |
| Indexed By | CPCI-S ; EI |
| Language | 英语 |
| Citation statistics | |
| Document Type | 会议论文 |
| Identifier | http://dspace.imech.ac.cn/handle/311007/58875 |
| Collection | 高温气体动力学国家重点实验室 |
| Corresponding Author | Wan, TA (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam LHD, Beijing 100190, Peoples R China. |
| Recommended Citation GB/T 7714 | 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. |
| Files in This Item: | ||||||
| File Name/Size | DocType | Version | Access | License | ||
| CPCI-Add024.pdf（468KB） | 会议论文 | 开放获取 | CC BY-NC-SA | View Application Full Text | ||
Items in the repository are protected by copyright, with all rights reserved, unless otherwise indicated.
Edit Comment