TY - GEN
T1 - Numerical study of oblique detonation initiations with chain branching kinetics
AU - Teng, Honghui
AU - Yang, Pengfei
AU - Jiang, Zonglin
N1 - Publisher Copyright:
© 2017 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
PY - 2017
Y1 - 2017
N2 - Oblique detonations induced by semi-infinite wedge are simulated by solving Euler equations with chain branching kinetics. Numerical results show the initiation can be triggered by either the abrupt transition or smooth transition, dependent on incident Ma Min and wedge angle θ, and then their effects on the oblique detonation angle β and initiation length Lini are analyzed. When θ increases, Lini decreases monotonically but β has a minimum value, corresponding to θ = 29° in this study. When Min decreases, both Lini and β increases monotonically until Min decreases below certain critical value, Min = 9.2 in this study. Then low inflow Ma effects generate the maximum Lini, with the complex of ODW (oblique detonation wave), SODW (secondary oblique detonation wave) and SIDW (self-ignition deflagration wave). The transient process is observed, demonstrating the structure can self-adjust to find a proper position. The wave structure suggests two wave/heat release process determining the detonation initiation. In the cases with high Min featured by SIDW, the oblique-shock induced self-ignition dominates, and Lini increases when Min decreases. In the cases with low Min featured by SODW, the interaction of ODW and SODW dominates, and Lini decreases when Min decreases.
AB - Oblique detonations induced by semi-infinite wedge are simulated by solving Euler equations with chain branching kinetics. Numerical results show the initiation can be triggered by either the abrupt transition or smooth transition, dependent on incident Ma Min and wedge angle θ, and then their effects on the oblique detonation angle β and initiation length Lini are analyzed. When θ increases, Lini decreases monotonically but β has a minimum value, corresponding to θ = 29° in this study. When Min decreases, both Lini and β increases monotonically until Min decreases below certain critical value, Min = 9.2 in this study. Then low inflow Ma effects generate the maximum Lini, with the complex of ODW (oblique detonation wave), SODW (secondary oblique detonation wave) and SIDW (self-ignition deflagration wave). The transient process is observed, demonstrating the structure can self-adjust to find a proper position. The wave structure suggests two wave/heat release process determining the detonation initiation. In the cases with high Min featured by SIDW, the oblique-shock induced self-ignition dominates, and Lini increases when Min decreases. In the cases with low Min featured by SODW, the interaction of ODW and SODW dominates, and Lini decreases when Min decreases.
UR - http://www.scopus.com/inward/record.url?scp=85017272580&partnerID=8YFLogxK
U2 - 10.2514/6.2017-1287
DO - 10.2514/6.2017-1287
M3 - Conference contribution
AN - SCOPUS:85017272580
T3 - AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting
BT - AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting
PB - American Institute of Aeronautics and Astronautics Inc.
T2 - 55th AIAA Aerospace Sciences Meeting
Y2 - 9 January 2017 through 13 January 2017
ER -