| contributor author | Wei Huang | |
| contributor author | Lin Ma | |
| contributor author | Mohamed Pourkashanian | |
| contributor author | Derek B. Ingham | |
| contributor author | Shi-bin Luo | |
| contributor author | Jun Liu | |
| contributor author | Zhen-guo Wang | |
| date accessioned | 2017-05-08T21:33:51Z | |
| date available | 2017-05-08T21:33:51Z | |
| date copyright | July 2012 | |
| date issued | 2012 | |
| identifier other | %28asce%29as%2E1943-5525%2E0000136.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/56281 | |
| description abstract | As one of the most promising propulsive systems for future hypersonic vehicles, the hydrogen-fueled dual-mode scramjet combustor has drawn the attention of an ever increasing number of researchers. The two-dimensional coupled implicit NS equations, the standard | |
| publisher | American Society of Civil Engineers | |
| title | Flow-Field Analysis of a Typical Hydrogen-Fueled Dual-Mode Scramjet Combustor | |
| type | Journal Paper | |
| journal volume | 25 | |
| journal issue | 3 | |
| journal title | Journal of Aerospace Engineering | |
| identifier doi | 10.1061/(ASCE)AS.1943-5525.0000136 | |
| tree | Journal of Aerospace Engineering:;2012:;Volume ( 025 ):;issue: 003 | |
| contenttype | Fulltext | |
