TY - JOUR
T1 - 点火方式对空桶型旋转爆震燃烧室起爆特性的影响
AU - Zhao, Minghao
AU - Wang, Ke
AU - Wang, Zhicheng
AU - Zhu, Yiyuan
AU - Yu, Xiaodong
AU - Fan, Wei
N1 - Publisher Copyright:
© 2022, Beihang University Aerospace Knowledge Press. All right reserved.
PY - 2022/1/25
Y1 - 2022/1/25
N2 - To investigate the initiation process and operating characteristics of rotating detonation waves in the hollow combustor, the initiation and propagation of rotating detonation waves of three ignition methods, i.e., spark plug ignition, vertical pre-detonation tube ignition, and tangential pre-detonation tube ignition, were studied. Ethylene and oxygen-enriched air were used as fuel and oxidizer, respectively. Experimental results indicate that the rotating detonation waves were able to be initiated and propagated steadily with the three ignition methods, which seem to have little influence on the propagating direction of rotating detonation waves. Compared with the results of spark plug ignition, stable detonations were available with a wider range of mass flow rate when adopting vertical and tangential pre-detonation tube ignition. The obtained average propagating velocities of rotating detonations were almost consistent for all the three cases. When the pre-detonation tube was used, the initiation time of rotating detonation wave was obviously shorter and less discrete than that of spark plug ignition.
AB - To investigate the initiation process and operating characteristics of rotating detonation waves in the hollow combustor, the initiation and propagation of rotating detonation waves of three ignition methods, i.e., spark plug ignition, vertical pre-detonation tube ignition, and tangential pre-detonation tube ignition, were studied. Ethylene and oxygen-enriched air were used as fuel and oxidizer, respectively. Experimental results indicate that the rotating detonation waves were able to be initiated and propagated steadily with the three ignition methods, which seem to have little influence on the propagating direction of rotating detonation waves. Compared with the results of spark plug ignition, stable detonations were available with a wider range of mass flow rate when adopting vertical and tangential pre-detonation tube ignition. The obtained average propagating velocities of rotating detonations were almost consistent for all the three cases. When the pre-detonation tube was used, the initiation time of rotating detonation wave was obviously shorter and less discrete than that of spark plug ignition.
KW - Hollow combustor
KW - Ignition
KW - Initiation process
KW - Propagating direction
KW - Rotating detonation
UR - http://www.scopus.com/inward/record.url?scp=85124245209&partnerID=8YFLogxK
U2 - 10.7527/S1000-6893.2020.24870
DO - 10.7527/S1000-6893.2020.24870
M3 - 文章
AN - SCOPUS:85124245209
SN - 1000-6893
VL - 43
JO - Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
JF - Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
IS - 1
M1 - 124870
ER -