TY - JOUR
T1 - The flame propagation characteristics and detonation parameters of ammonia/oxygen in a large-scale horizontal tube
T2 - As a carbon-free fuel and hydrogen-energy carrier
AU - Jing, Qi
AU - Huang, Jinxiang
AU - Liu, Qingming
AU - wang, Dan
AU - Chen, Xu
AU - Wang, Zhisong
AU - Liu, Changqi
N1 - Publisher Copyright:
© 2021 Hydrogen Energy Publications LLC
PY - 2021/5/25
Y1 - 2021/5/25
N2 - As a carbon-free fuel and a hydrogen-energy carrier, ammonia is a potential candidate for future energy utilization. Therefore, in order to promote the application of ammonia in detonation engines and to evaluate the safety of ammonia related industrial process, DDT experiments for ammonia/oxygen mixtures with different ERs were carried out in a large-scale horizontal tube. Moreover, pressure transducers and self-developed temperature sensors were applied to record the overpressure and the instantaneous flame temperature during DDT process. The results show that the DDT process in ammonia/oxygen mixtures contains four stages: Slow propagation stage, Flame and pressure wave acceleration stage, Fast propagation and detonation wave formation stage, Detonation wave self-sustained propagation stage. For stoichiometric ammonia/oxygen mixtures, flame front and the leading shock wave propagate one after another with different velocity, until they closely coupled and propagated together with one steady velocity. At the same time, it is found that an interesting retonation wave propagates backward. The peak overpressure, detonation velocity, and flame temperature of the self-sustained detonation are 2 MPa, 2000 m/s and 3500 K, respectively. With the ER increased from 0.6 to 1.6, the detonation velocities and peak overpressures ranged from 2310 m/s to 2480 m/s and 25.6 bar–28.7 bar, respectively. In addition, the detonation parameters of ammonia were compared with those of methane and hydrogen to evaluate the detonation performance and destructiveness of ammonia.
AB - As a carbon-free fuel and a hydrogen-energy carrier, ammonia is a potential candidate for future energy utilization. Therefore, in order to promote the application of ammonia in detonation engines and to evaluate the safety of ammonia related industrial process, DDT experiments for ammonia/oxygen mixtures with different ERs were carried out in a large-scale horizontal tube. Moreover, pressure transducers and self-developed temperature sensors were applied to record the overpressure and the instantaneous flame temperature during DDT process. The results show that the DDT process in ammonia/oxygen mixtures contains four stages: Slow propagation stage, Flame and pressure wave acceleration stage, Fast propagation and detonation wave formation stage, Detonation wave self-sustained propagation stage. For stoichiometric ammonia/oxygen mixtures, flame front and the leading shock wave propagate one after another with different velocity, until they closely coupled and propagated together with one steady velocity. At the same time, it is found that an interesting retonation wave propagates backward. The peak overpressure, detonation velocity, and flame temperature of the self-sustained detonation are 2 MPa, 2000 m/s and 3500 K, respectively. With the ER increased from 0.6 to 1.6, the detonation velocities and peak overpressures ranged from 2310 m/s to 2480 m/s and 25.6 bar–28.7 bar, respectively. In addition, the detonation parameters of ammonia were compared with those of methane and hydrogen to evaluate the detonation performance and destructiveness of ammonia.
KW - Ammonia
KW - Deflagration to detonation transition (DDT)
KW - Detonation parameters
KW - Flame acceleration
UR - http://www.scopus.com/inward/record.url?scp=85103543294&partnerID=8YFLogxK
U2 - 10.1016/j.ijhydene.2021.03.032
DO - 10.1016/j.ijhydene.2021.03.032
M3 - Article
AN - SCOPUS:85103543294
SN - 0360-3199
VL - 46
SP - 19158
EP - 19170
JO - International Journal of Hydrogen Energy
JF - International Journal of Hydrogen Energy
IS - 36
ER -