TY - GEN
T1 - An experimental study on the deflagration-to-detonation transition in millimeter scale tubes
AU - He, Jiannan
AU - Fan, Wei
AU - Chi, Yeqing
N1 - Publisher Copyright:
© 2016, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2016
Y1 - 2016
N2 - The deflagration-to-detonation transition of ethylene-oxygen mixture was studied in thin tubes with inner diameters of 2, 4 and 8 mm. To better make the experiment comparable to the previous simulation configuration, the flames were ignited from stationary state which conforms to the precondition of closed-end ignition. Flame speeds and other parameters were measured using high speed camera. The characteristics of pre-detonation acceleration were analyzed both qualitatively and quantitatively. It is concluded that, unlike the results that the numerical researches have found, there are four distinctive acceleration stages during the DDT process. In thinner tubes, flames propagate faster, while the characteristic acceleration time is shorter in larger tubes. The sound speed of the burned and unburned gas is considered to be the critical velocity, beyond which the flame may be boosted more quickly to detonation. When the saturation speed in the third acceleration stage becomes supersonic in larger tubes, the DDT distance may be shortened.
AB - The deflagration-to-detonation transition of ethylene-oxygen mixture was studied in thin tubes with inner diameters of 2, 4 and 8 mm. To better make the experiment comparable to the previous simulation configuration, the flames were ignited from stationary state which conforms to the precondition of closed-end ignition. Flame speeds and other parameters were measured using high speed camera. The characteristics of pre-detonation acceleration were analyzed both qualitatively and quantitatively. It is concluded that, unlike the results that the numerical researches have found, there are four distinctive acceleration stages during the DDT process. In thinner tubes, flames propagate faster, while the characteristic acceleration time is shorter in larger tubes. The sound speed of the burned and unburned gas is considered to be the critical velocity, beyond which the flame may be boosted more quickly to detonation. When the saturation speed in the third acceleration stage becomes supersonic in larger tubes, the DDT distance may be shortened.
UR - http://www.scopus.com/inward/record.url?scp=85088200345&partnerID=8YFLogxK
U2 - 10.2514/6.2016-5107
DO - 10.2514/6.2016-5107
M3 - 会议稿件
AN - SCOPUS:85088200345
SN - 9781624104060
T3 - 52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016
BT - 52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016
Y2 - 25 July 2016 through 27 July 2016
ER -