Effects of a turbine guide vane on hydrogen-air rotating detonation wave propagation characteristics
Effects of a turbine guide vane on hydrogen-air rotating detonation wave propagation characteristics
复制标题
涡轮导叶对氢-空气旋转爆震波传播特性的影响
DOI:
10.1016/j.ijhydene.2017.06.115
复制
发表时间:
2017-08
影响因子:
7.2
通讯作者:
Zhou Changsheng
中科院分区:
文献类型:
--
作者:
Zhou Shengbing;Ma Hu;Li Shuai;Liu Daokun;Yan Yu;Zhou Changsheng
The rotating detonation engine is a new machine that can generate thrust via continuous rotating detonation waves (RDWs). In this study, experiments were performed on a structure combining a rotating detonation combustor (RDC) and a turbine guide vane to investigate the propagation characteristic of hydrogen-air RDW. The results showed that the velocity of detonation wave initially increased and then decreased with the increase of equivalence ratio, and it got a velocity of 84% Chapman-Jouguet value. The velocity of detonation wave generally rose by 4.31% comparing with the no guide vane tests, while the scope of steady-operation state became narrow. The oscillation pressure was reduced by 64% after passing through the guide vane, and the magnitude of pressure was only 0.4 bar at the guide vane exit. Meanwhile, part of the shock wave was reflected back to combustor resulting in some small pressure disturbances, and the propagation mode of reflected wave was related to the propagation direction of RDW.
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影响因子:
7.2
作者:
R. Driscoll;Paul Aghasi;A. S. George;E. Gutmark
通讯作者:
R. Driscoll;Paul Aghasi;A. S. George;E. Gutmark
影响因子:
7.2
作者:
V. Anand;A. S. George;R. Driscoll;E. Gutmark
通讯作者:
V. Anand;A. S. George;R. Driscoll;E. Gutmark
DOI:
10.2514/6.2013-1030
发表时间:
2013-01
期刊:
Optics & Laser Technology
影响因子:
--
作者:
Nick D DeBarmore;P. King;F. Schauer;J. Hoke
通讯作者:
Nick D DeBarmore;P. King;F. Schauer;J. Hoke
DOI:
10.2514/6.2014-1316
发表时间:
2014-01
期刊:
--
影响因子:
--
作者:
Dan Welsh;P. King;F. Schauer;J. Hoke
通讯作者:
Dan Welsh;P. King;F. Schauer;J. Hoke
影响因子:
5.1
作者:
Q. Zheng;C. Weng;Q. Bai
通讯作者:
Q. Zheng;C. Weng;Q. Bai