| contributor author | Wen Bao | |
| contributor author | Jichao Hu | |
| contributor author | Youhai Zong | |
| contributor author | Qingchun Yang | |
| contributor author | Juntao Chang | |
| contributor author | Meng Wu | |
| contributor author | Daren Yu | |
| date accessioned | 2017-05-08T21:34:21Z | |
| date available | 2017-05-08T21:34:21Z | |
| date copyright | September 2014 | |
| date issued | 2014 | |
| identifier other | %28asce%29as%2E1943-5525%2E0000331.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/56480 | |
| description abstract | The ignition characteristics of a flush wall, liquid-kerosene-fueled scramjet combustor are tested in a directly connected ground test rig. The total temperature and Mach number of the vitiated airflow at the exit of the nozzle are 1,505 K and 3.0, respectively. The ignition process is accomplished by air throttling and a micro hot gas generator (MHGG). Without any cavity or backward steps, the flame holding is also accomplished by the MHGG. By controlling the air-throttling pressure and overlap time of the air throttling and the MHGG, different ignition results can be achieved. This paper divides these different results into four ignition modes and provides a detailed description of the characteristics of each mode. In addition, this paper summarizes the experiment data and proves that the ignition laws have some relationship to the fuel–air equivalence ratio. | |
| publisher | American Society of Civil Engineers | |
| title | Ignition Characteristics of a Liquid-Kerosene-Fueled Scramjet during Air Throttling Combined with a Gas Generator | |
| type | Journal Paper | |
| journal volume | 27 | |
| journal issue | 5 | |
| journal title | Journal of Aerospace Engineering | |
| identifier doi | 10.1061/(ASCE)AS.1943-5525.0000329 | |
| tree | Journal of Aerospace Engineering:;2014:;Volume ( 027 ):;issue: 005 | |
| contenttype | Fulltext | |
