TY - JOUR
T1 - Deflagration to detonation transition characteristic in U-bend square tube
AU - Wang, Wei
AU - Qiu, Hua
AU - Fan, Wei
AU - Xiong, Cha
PY - 2014/8/1
Y1 - 2014/8/1
N2 - To shorten the axial length of detonation tube, a practicable way was used by replacing straight detonation tube with a curve one. A series of two-dimensional numerical simulations were performed in U-bend square tubes, and the effect laws of ignition position, ignition energy, inner radius of bend-section on formation and diffusion of detonation wave were studied. The simulation results show that the deflagration to detonation transition (DDT) time reduces with the increase of inner radius of bend-section; when the inner radius of bend-section is the maximum, the DDT distance is the shortest; the increasing ignition energy means the increasing shock wave strength in detonation tube and the decreasing DDT time; when the ignition position is set at 300 mm after the inlet of the detonation tube, the peak pressure of detonation wave is the highest, and the DDT time is the shortest.
AB - To shorten the axial length of detonation tube, a practicable way was used by replacing straight detonation tube with a curve one. A series of two-dimensional numerical simulations were performed in U-bend square tubes, and the effect laws of ignition position, ignition energy, inner radius of bend-section on formation and diffusion of detonation wave were studied. The simulation results show that the deflagration to detonation transition (DDT) time reduces with the increase of inner radius of bend-section; when the inner radius of bend-section is the maximum, the DDT distance is the shortest; the increasing ignition energy means the increasing shock wave strength in detonation tube and the decreasing DDT time; when the ignition position is set at 300 mm after the inlet of the detonation tube, the peak pressure of detonation wave is the highest, and the DDT time is the shortest.
KW - Deflagration
KW - Deflagration to detonation transition
KW - Detonation
KW - Pulse detonation engine
KW - U-bend square tube
UR - http://www.scopus.com/inward/record.url?scp=84906736395&partnerID=8YFLogxK
U2 - 10.13224/j.cnki.jasp.2014.08.006
DO - 10.13224/j.cnki.jasp.2014.08.006
M3 - 文章
AN - SCOPUS:84906736395
SN - 1000-8055
VL - 29
SP - 1796
EP - 1801
JO - Hangkong Dongli Xuebao/Journal of Aerospace Power
JF - Hangkong Dongli Xuebao/Journal of Aerospace Power
IS - 8
ER -