TY - JOUR
T1 - Simulation and analysis of wall heat fluxes for shear coaxial GH 2/GO 2 single element combustor
AU - Jiang, Jin Peng
AU - Li, Mao
AU - Jin, Ping
AU - Cai, Guo Biao
PY - 2012/8
Y1 - 2012/8
N2 - With gas hydrogen/gas oxygen being propellant, adopting numerical simulation, design parameters of shear coaxial injector, namely ratio of fuel velocity to oxidizer velocity and the ratio of oxidizer pressure drop to combustor pressure have been studied to find their impact on combustion characteristics and thermal loading of chamber wall. The simulation results of two kinds of wall boundary condition which were adiabat condition and isothermal condition were compared with experimental result. It shows that the increasing of the ratio of fuel velocity to oxidizer velocity improves the combustion performance and wall heat flux. The increasing of the ratio of oxidizer pressure drop to combustor pressure decreases the combustion performance and wall heat flux. In comparison with wall gas temperature, wall heat flux is more consistent with the real condition when used to predict thermal loading of combustion chamber wall.
AB - With gas hydrogen/gas oxygen being propellant, adopting numerical simulation, design parameters of shear coaxial injector, namely ratio of fuel velocity to oxidizer velocity and the ratio of oxidizer pressure drop to combustor pressure have been studied to find their impact on combustion characteristics and thermal loading of chamber wall. The simulation results of two kinds of wall boundary condition which were adiabat condition and isothermal condition were compared with experimental result. It shows that the increasing of the ratio of fuel velocity to oxidizer velocity improves the combustion performance and wall heat flux. The increasing of the ratio of oxidizer pressure drop to combustor pressure decreases the combustion performance and wall heat flux. In comparison with wall gas temperature, wall heat flux is more consistent with the real condition when used to predict thermal loading of combustion chamber wall.
KW - Combustion performance
KW - Gas hydrogen/gas oxygen injector
KW - Numerical simulation
KW - Ratio of fuel velocity to oxidizer velocity
KW - Ratio of oxidizer pressure drop to combustor pressure
KW - Wall thermal loading
UR - https://www.scopus.com/pages/publications/84867595656
M3 - 文章
AN - SCOPUS:84867595656
SN - 1000-8055
VL - 27
SP - 1881
EP - 1886
JO - Hangkong Dongli Xuebao/Journal of Aerospace Power
JF - Hangkong Dongli Xuebao/Journal of Aerospace Power
IS - 8
ER -