TY - JOUR
T1 - Numerical simulation on gas-liquid two-phase detonation combustion induced by shock wave focusing
AU - Yang, Qing
AU - Li, Zhi Qiang
AU - Di, Ya Chao
AU - Xu, Huan
PY - 2014/8/1
Y1 - 2014/8/1
N2 - Numerical simulation on gas-liquid two-phase detonation combustion of kerosene-air was conducted induced by shock wave focusing and setting obstacles. The numerical model of gas-liquid two-phase flow was established for the fuel injection, atomization and mixing of pulse detonation engine (PDE) by an Eulerian-Lagrangian formulation. Computational results show that the reflection and focusing of the ring shock wave can ignite the combustible mixture inside the capacity of detonation tube. Re-reflection and focusing of the reflecting shock wave could form higher temperature and pressure points (2 700 K, 25 MPa) near the obstacles, which can lead to local explosion, further generate stable pulse detonation combustion (velocity of 1 900 m/s, temperature of 2 950 K) and shorten the length of deflagration to detonation transition (DDT) to 0.45 m effectively.
AB - Numerical simulation on gas-liquid two-phase detonation combustion of kerosene-air was conducted induced by shock wave focusing and setting obstacles. The numerical model of gas-liquid two-phase flow was established for the fuel injection, atomization and mixing of pulse detonation engine (PDE) by an Eulerian-Lagrangian formulation. Computational results show that the reflection and focusing of the ring shock wave can ignite the combustible mixture inside the capacity of detonation tube. Re-reflection and focusing of the reflecting shock wave could form higher temperature and pressure points (2 700 K, 25 MPa) near the obstacles, which can lead to local explosion, further generate stable pulse detonation combustion (velocity of 1 900 m/s, temperature of 2 950 K) and shorten the length of deflagration to detonation transition (DDT) to 0.45 m effectively.
KW - Deflagration to detonation transition
KW - Detonation combustion
KW - Gas-liquid two-phase
KW - Pulse detonation engine
KW - Shock wave focusing
UR - https://www.scopus.com/pages/publications/84906777643
U2 - 10.13224/j.cnki.jasp.2014.08.007
DO - 10.13224/j.cnki.jasp.2014.08.007
M3 - 文章
AN - SCOPUS:84906777643
SN - 1000-8055
VL - 29
SP - 1802
EP - 1809
JO - Hangkong Dongli Xuebao/Journal of Aerospace Power
JF - Hangkong Dongli Xuebao/Journal of Aerospace Power
IS - 8
ER -