典型文献
Numerical study on ethylene-air continuous rotating detonation in annular combustors with different widths
文献摘要:
To investigate the impact of combustor width on continuous rotating detonation (CRD) fueled by ethylene and air, a series of 3D simulations are conducted by changing the inner cylinder radius of an annular combustor while retaining the same outer cylinder radius. The results show that the CRD wave propagates more steadily and faster as the combustor width increases. The high-temperature zone at the backward-facing step preheats the propellants and contributes to the steady propagation of the CRD wave in 25-and 30-mm wide combustors. The highest and the lowest velocities are obtained in the 30-and 15-mm wide combustors at, respectively, 1880.27 and 1681.01 m/s. On the other hand, the average thrust decreases as the combustor width increases. The highest thrust is obtained in the 15-mm wide combustor while the lowest is in the 30-mm wide combustor, at 758.06 and 525.93 N, respectively. Nevertheless, the thrust is much more stable in the 25-and 30-mm wide combustors than in the 15-and 20-mm wide combustors.
文献关键词:
中图分类号:
作者姓名:
Wei-jie FAN;Wei-dong LIU;Hao-yang PENG;Shi-jie LIU;Jian SUN
作者机构:
Science and Technology on Scramjet Laboratory,College of Aerospace Science and Technology,National University of Defense Technology,Changsha 410073,China;State Key Laboratory of Aerospace Dynamic,Satellite Control Center,Xi'an 710043,China
文献出处:
引用格式:
[1]Wei-jie FAN;Wei-dong LIU;Hao-yang PENG;Shi-jie LIU;Jian SUN-.Numerical study on ethylene-air continuous rotating detonation in annular combustors with different widths)[J].浙江大学学报(英文版)(A辑:应用物理和工程),2022(05):388-404
A类:
preheats
B类:
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AB值:
0.44772
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