关键词: 液氧;烃;液体推进剂火箭发动机;燃烧模拟

Abstract: A current mold el of combustion in LOX/hydrocarbon rocket engines is presented.Combustion processes are described with coupled stream tube mode. Specially,the effects of stripping of propellant droplets,supercritical combustion, and filmcooling on combustion are considered. With the model, the combustion processes in LOX/propane engines are simulated. The results show that the model provides an efficient method for simulation of combustion processes in LOX/ hydrocarbon rocket engines and for prediction of performance.

Key words: Liquid oxygen;Hydrocarbon;Liquid rocket engine;Combustion;Simulation