TY - JOUR
T1 - Initiation of oblique detonation waves induced by a blunt wedge in stoichiometric hydrogen-air mixtures
AU - Fang, Yishen
AU - Zhang, Zijian
AU - Hu, Zongmin
AU - Deng, Xi
N1 - Funding Information:
The research is supported by the Natural Science Foundation of China (grant numbers 11672308 , 11532014 ).
Publisher Copyright:
© 2019 Elsevier Masson SAS
PY - 2019/9
Y1 - 2019/9
N2 - Two-dimensional, oblique detonation waves (ODWs) in a stoichiometric hydrogen-air mixture are simulated with the reactive Euler equations using a detailed chemical reaction model. This study focuses on blunt wedge induced ODWs, which are not only influenced by inflow parameters but also the size of the blunt body. With the inflow parameters of flight altitude of 30 km and flight Mach number M0 of 8-10, the numerical results demonstrate that the blunt wedge is crucial to initiate the ODW. In the case of M0=10, the straight wedge without the blunt forebody can initiate the detonation. However, decreasing M0 causes the failure of initiation, which can be compensated by increasing the radius R0 of the blunt forebody. By adjusting R0, two initiation procedures are observed and distinguished: one is the wedge-induced initiation and the other is the blunt forebody-induced initiation. Although both have been independently studied before, in this study, their coexistence is demonstrated, and the mechanism is analyzed for the first time. A theoretical analysis based on the classic initiation theory is performed to elucidate the initiation mechanism, giving a good agreement between the critical radius with numerical results.
AB - Two-dimensional, oblique detonation waves (ODWs) in a stoichiometric hydrogen-air mixture are simulated with the reactive Euler equations using a detailed chemical reaction model. This study focuses on blunt wedge induced ODWs, which are not only influenced by inflow parameters but also the size of the blunt body. With the inflow parameters of flight altitude of 30 km and flight Mach number M0 of 8-10, the numerical results demonstrate that the blunt wedge is crucial to initiate the ODW. In the case of M0=10, the straight wedge without the blunt forebody can initiate the detonation. However, decreasing M0 causes the failure of initiation, which can be compensated by increasing the radius R0 of the blunt forebody. By adjusting R0, two initiation procedures are observed and distinguished: one is the wedge-induced initiation and the other is the blunt forebody-induced initiation. Although both have been independently studied before, in this study, their coexistence is demonstrated, and the mechanism is analyzed for the first time. A theoretical analysis based on the classic initiation theory is performed to elucidate the initiation mechanism, giving a good agreement between the critical radius with numerical results.
KW - Blunt wedge
KW - Hydrogen
KW - Initiation
KW - Oblique detonation wave
UR - http://www.scopus.com/inward/record.url?scp=85068385647&partnerID=8YFLogxK
U2 - 10.1016/j.ast.2019.06.031
DO - 10.1016/j.ast.2019.06.031
M3 - Journal article
AN - SCOPUS:85068385647
SN - 1270-9638
VL - 92
SP - 676
EP - 684
JO - Aerospace Science and Technology
JF - Aerospace Science and Technology
ER -