TY - JOUR
T1 - 燃油初温对两相爆震性能影响的实验研究
AU - Wang, Yong Jia
AU - Yan, Yu
AU - Zhang, Yang
AU - Fan, Wei
AU - Zhang, Qi Bin
AU - Jiao, Zhong Tian
N1 - Publisher Copyright:
© 2021, Editorial Department of Journal of Propulsion Technology. All right reserved.
PY - 2021/4
Y1 - 2021/4
N2 - To investigate the effects of initial fuel temperature on the performance of two-phase detonation, experiments under different fuel temperature conditions from 30℃ to 200℃ were conducted in a 24mm detonation tube at 10Hz, utilizing kerosene and oxygen as fuel and oxidant, respectively. The results show that, with the rise of the initial temperature of fuel, the steady propagation velocity of the flame front increases gradually, the combustion stability increases, the two-phase detonation peak pressure increases, the detonation initiation distance reduces. In addition, the observation of detonation tail flame at different initial fuel temperatures shows that, with the increase of fuel temperature, both the total pressure of unsteady exhaust process and the thrust available for the engine increase.
AB - To investigate the effects of initial fuel temperature on the performance of two-phase detonation, experiments under different fuel temperature conditions from 30℃ to 200℃ were conducted in a 24mm detonation tube at 10Hz, utilizing kerosene and oxygen as fuel and oxidant, respectively. The results show that, with the rise of the initial temperature of fuel, the steady propagation velocity of the flame front increases gradually, the combustion stability increases, the two-phase detonation peak pressure increases, the detonation initiation distance reduces. In addition, the observation of detonation tail flame at different initial fuel temperatures shows that, with the increase of fuel temperature, both the total pressure of unsteady exhaust process and the thrust available for the engine increase.
KW - Distance of deflagration to detonation transition
KW - Initial temperature of fuel
KW - Mach disk
KW - Total pressure of exhaust gas
KW - Wave velocity
UR - http://www.scopus.com/inward/record.url?scp=85104749264&partnerID=8YFLogxK
U2 - 10.13675/j.cnki.tjjs.200630
DO - 10.13675/j.cnki.tjjs.200630
M3 - 文章
AN - SCOPUS:85104749264
SN - 1001-4055
VL - 42
SP - 892
EP - 897
JO - Tuijin Jishu/Journal of Propulsion Technology
JF - Tuijin Jishu/Journal of Propulsion Technology
IS - 4
ER -